L-band Digital Aeronautical Communications System (LDACS)

Internet-Draft	LDACS	December 2022
Mäurer, et al.	Expires 5 June 2023	[Page]

Abstract

This document gives an overview of the architecture of the L-band Digital Aeronautical Communications System (LDACS), which provides a secure, scalable and spectrum efficient terrestrial data link for civil aviation. LDACS is a scheduled, reliable multi-application cellular broadband system with support for IPv6. It is part of a larger shift of flight guidance communication moving to IP-based communication. High reliability and availability of IP connectivity over LDACS, as well as security, are therefore essential. The intent of this document is to introduce LDACS to the IETF community, raise awareness on related activities inside and outside of the IETF, and to seek expertise in shaping the shift of aeronautics to IP.¶

1. Introduction

One of the main pillars of the modern Air Traffic Management (ATM) system is the existence of a communications infrastructure that enables efficient aircraft control and safe aircraft separation in all phases of flight. Current systems are technically mature but suffering from the Very High Frequency (VHF) band's increasing saturation in high-density areas and the limitations posed by analogue radio communications. Therefore, aviation strives for a sustainable modernization of the aeronautical communications infrastructure on the basis of IP.¶

This modernization is realized in two steps: (1) the transition of communications datalinks from analogue to digital technologies and, (2) the introduction of IPv6 based networking protocols [RFC8200] in aeronautical networks [ICAO2015].¶

Step (1) is realized via ATM communications transitioning from analogue VHF voice [KAMA2010] to more spectrum efficient digital data communication. For terrestrial communications the International Civil Aviation Organization (ICAO)'s Global Air Navigation Plan (GANP) foresees this transition to be realized by the development of the L-band Digital Aeronautical Communications System (LDACS). Since Central Europe has been identified as the area of the world that suffers the most from increased saturation of the VHF band, the initial roll-out of LDACS will likely start there, and continue to other increasingly saturated zones as the East and West Coast of the US and parts of Asia [ICAO2018].¶

Technically LDACS enables IPv6-based air-ground communication related to aviation safety and regularity of flight [ICAO2015]. Passenger communication and similar services are not supported, since only communications related to "safety and regularity of flight" are permitted in protected aviation frequency bands. The particular challenge is that no additional frequencies can be made available for terrestrial aeronautical communication. It was thus necessary to develop co-existence mechanism/procedures to enable the interference free operation of LDACS in parallel with other aeronautical services/systems in the protected frequency band. Since LDACS will be used for aircraft guidance, high reliability and availability for IP connectivity over LDACS are essential.¶

LDACS is standardized in ICAO and European Organization for Civil Aviation Equipment (EUROCAE).¶

This document provides information to the IETF community about the aviation industry transition of flight guidance systems from analog to digital, provides context for LDACS relative to related IETF activities [I-D.haindl-lisp-gb-atn], and seeks expertise on realizing reliable IPv6 over LDACS for step (1). This document does not intend to advance LDACS as an IETF standards-track document.¶

Step (2) is a strategy for the worldwide roll-out of IPv6 capable digital aeronautical inter-networking. This is called the Aeronautical Telecommunications Network (ATN)/Internet Protocol Suite (IPS) (hence, ATN/IPS). It is specified in the International Civil Aviation Organization (ICAO) document Doc 9896 [ICAO2015], the Radio Technical Commission for Aeronautics (RTCA) document DO-379 [RTCA2019], the EUROCAE document ED-262 [EURO2019], and the Aeronautical Radio Incorporated (ARINC) document P858 [ARI2021]. LDACS is subject to these regulations since it provides an "access network" - link-layer datalink - to the ATN/IPS.¶

ICAO has chosen IPv6 as basis for the ATN/IPS mostly for historical reasons, since a previous architecture based on ISO/OSI protocols, the ATN/OSI, failed in the marketplace.¶

In the context of safety-related communications, LDACS will play a major role in future ATM. ATN/IPS datalinks will provide diversified terrestrial and space-based connectivity in a multilink concept, called the Future Communications Infrastructure (FCI) [VIR2021]. From a technical point of view the FCI will realize airborne multi-homed IPv6 networks connected to a global ground network via at least two independent communication technologies. This is considered in more detail in related IETF work in progress [I-D.haindl-lisp-gb-atn] [I-D.ietf-rtgwg-atn-bgp]. As such, ICAO has actively sought out the support of IETF to define a mobility solution for step (2), which is currently the Locator/ID Separation Protocol (LISP).¶

In the context of the Reliable and Available Wireless (RAW) working group, developing options, such as intelligent switching between datalinks, for reliably delivering content from and to endpoints, is foreseen. As LDACS is part of such a concept, the work of RAW is immediately applicable. In general, with the aeronautical communications system transitioning to ATN/IPS, and data being transported via IPv6, closer cooperation and collaboration between the aeronautical and IETF community is desirable.¶

LDACS standardization within the framework of ICAO started in December 2016. The ICAO standardization group has produced the final Standards and Recommended Practices (SARPS) document as of 2022 [ICAO2022]. It defines the general characteristics of LDACS. By the end of 2023, the ICAO standardization group plans to have developed an ICAO technical manual - the ICAO equivalent to a technical standard. As such LDACS standardization is not finished yet, and therefore this document is a snapshot of current status. The physical characteristics of an LDACS installation (form, fit, and function) will be standardized by EUROCAE. Generally, the group is open to input from all sources and encourages cooperation between the aeronautical and the IETF community.¶

3. Motivation and Use Cases

Aircraft are currently connected to Air Traffic Control (ATC) and Aeronautical Operational Control (AOC) services via voice and data communications systems through all phases of flight. ATC refers to communication for flight guidance. AOC is a generic term referring to the business communication of airlines. It refers to the mostly proprietary exchange of data between the aircraft of the airline and the airline's operation centers and service partners. The ARINC document 633 was developed and first released in 2007 [ARI2019] with the goal to standardize these messages for interoperability, e.g., messages between the airline and fueling or de-icing companies. Within the airport and terminal area, connectivity is focused on high bandwidth communications. In the En-Route domain, however, high reliability, robustness, and range are the main foci. Voice communications may use the same or different equipment as data communications systems. In the following, the main differences between voice and data communications capabilities are summarized. The assumed list of use cases for LDACS complements the list of use cases stated in [RAW-USE-CASES] and the list of reliable and available wireless technologies presented in [RAW-TECHNOS].¶

3.1. Voice Communications Today

Voice links are used for Air/Ground (A/G) and Air/Air (A/A) communications. The communications equipment can be installed on ground or in the aircraft, in which cases the High Frequency (HF) or VHF frequency band is used. For remote domains voice communications can also be satellite-based. All VHF and HF voice communications are operated via open broadcast channels without authentication, encryption or other protective measures. The use of well-proven communications procedures via broadcast channels, such as phraseology or read-backs, requiring well-trained personnel, help to enhance the safety of communications, but does not replace necessary cryptographical security mechanisms. The main voice communications media is still the analogue VHF Double Side-Band Amplitude Modulation (DSB-AM) communications technique, supplemented by HF single side-band amplitude modulation and satellite communications for remote and oceanic regions. DSB-AM has been in use since 1948, works reliably and safely, and uses low-cost communication equipment. These are the main reasons why VHF DSB-AM communications are still in use, and it is likely that this technology will remain in service for many more years. This however, results in current operational limitations and impediments in deploying new ATM applications, such as flight-centric operation with point-to-point communications between pilots and air traffic control officers. [BOE2019]¶

3.2. Data Communications Today

Like for voice, data communications into the cockpit, are currently provided by ground-based equipment operating either on HF or VHF radio bands or by legacy satellite systems. All these communication systems use narrowband radio channels with a data throughput capacity in the order of kbit/s. While the aircraft is on the ground, some additional communications systems are available, like the Aeronautical Mobile Airport Communications System (AeroMACS) or public cellular networks, operating in the Airport (APT) domain and able to deliver broadband communications capability. [BOE2019]¶

For regulatory reasons, the data communications networks, used for the transmission of data relating to the safety and regularity of flight, must be strictly isolated from those providing entertainment services to passengers. This leads to a situation that the flight crews are supported by narrowband services during flight while passengers have access to inflight broadband services. The current HF and VHF data links cannot provide broadband services now or in the future, due to the lack of available spectrum. This technical shortcoming is becoming a limitation to enhanced ATM operations, such as trajectory-based operations and 4D trajectory negotiations. [BOE2019]¶

Satellite-based communications are currently under investigation and enhanced capabilities are under development which will be able to provide inflight broadband services and communications supporting the safety and regularity of flight. In parallel the ground-based broadband data link technology LDACS is being standardized by ICAO and has recently shown its maturity during flight tests [MAE20211] [BEL2021]. The LDACS technology is scalable, secure and spectrum efficient and provides significant advantages to the users and service providers. It is expected that both - satellite systems and LDACS - will be deployed to support the future aeronautical communication needs as envisaged by the ICAO Global Air Navigation Plan (GNAP). [BOE2019]¶

5. Applicability

LDACS is a multi-application cellular broadband system capable of simultaneously providing various kinds of Air Traffic Services (ATS) including ATS-B3, and AOC communications services from deployed Ground-Stations (GS). The physical layer and data link layer of LDACS are optimized for controller-pilot data link communications, but the system also supports digital air-ground voice communications.¶

LDACS supports communications in all airspaces (airport, terminal maneuvering area, and en-route), and on the airport surface. The physical LDACS cell coverage is effectively de-coupled from the operational coverage required for a particular service. This is new in aeronautical communications. Services requiring wide-area coverage can be installed at several adjacent LDACS cells. The handover between the involved LDACS cells is seamless, automatic, and transparent to the user. Therefore, the LDACS communications concept enables the aeronautical communication infrastructure to support future dynamic airspace management concepts.¶

5.1. Advances Beyond the State-of-the-Art

LDACS will offer several capabilities, not yet provided in contemporarily deployed aeronautical communications systems. All these were already tested and confirmed in lab or flight trials with available LDACS prototype hardware [BEL2021] [MAE20211].¶

5.1.1. Priorities

LDACS is able to manage service priorities, an important feature not available in some of the current data link deployments. Thus, LDACS guarantees bandwidth availability, low latency, and high continuity of service for safety critical ATS applications while simultaneously accommodating less safety-critical AOC services.¶

5.1.2. Security

LDACS is a secure data link with built-in security mechanisms. It enables secure data communications for ATS and AOC services, including secured private communications for aircraft operators and Air traffic Network Service Providers (ANSP). This includes concepts for key and trust management, mutual authentication and key establishment protocols, key derivation measures, user and control message-in-transit protection, secure logging and availability and robustness measures [MAE20182] [MAE2021].¶

5.1.3. High Data Rates

The user data rate of LDACS is 315 kbit/s to 1428 kbit/s on the Forward Link (FL) for the Ground-to-Air (G2A) connection, and 294 kbit/s to 1390 kbit/s on the Reverse Link (RL) for the Air-to-Ground (A2G) connection, depending on coding and modulation. This is up to two orders of magnitude greater than current terrestrial digital aeronautical communications systems, such as the VHF Data Link mode 2 (VDLm2), provide [ICAO2019] [GRA2020].¶

5.2. Application

LDACS will be used by several aeronautical applications ranging from enhanced communications protocol stacks (multi-homed mobile IPv6 networks in the aircraft and potentially ad-hoc networks between aircraft) to broadcast communication applications (GNSS correction data) and integration with other service domains (using the communications signal for navigation) [MAE20211]. Also, a digital voice service offering better quality and service than current HF and VHF systems is foreseen.¶

5.2.1. Air/Ground Multilink

It is expected that LDACS, together with upgraded satellite-based communications systems, will be deployed within the FCI and constitute one of the main components of the multilink concept within the FCI.¶

Both technologies, LDACS and satellite systems, have their specific benefits and technical capabilities which complement each other. Especially, satellite systems are well-suited for large coverage areas with less dense air traffic, e.g. oceanic regions. LDACS is well-suited for dense air traffic areas, e.g., continental areas or hot-spots around airports and terminal airspace. In addition, both technologies offer comparable data link capacity and, thus, are well-suited for redundancy, mutual back-up, or load balancing.¶

Technically the FCI multilink concept will be realized by multi-homed mobile IPv6 networks in the aircraft. The related protocol stack is currently under development by ICAO, within SESAR, and the IETF. Currently two layers of mobility are foreseen. Local mobility within the LDACS access network is realized through PMIPv6, global mobility between "multi-link" access networks (which need not be LDACS) is implemented on top of LISP [I-D.haindl-lisp-gb-atn] [I-D.ietf-lisp-rfc6830bis] [I-D.ietf-lisp-rfc6833bis].¶

5.2.2. Air/Air Extension for LDACS

A potential extension of the multilink concept is its extension to the integration of ad-hoc networks between aircraft.¶

Direct A/A communication between aircraft in terms of ad-hoc data networks are currently considered a research topic since there is no immediate operational need for it, although several possible use cases are discussed (Automatic Dependent Surveillance - Broadcast (ADS-B), digital voice, wake vortex warnings, and trajectory negotiation) [BEL2019]. It should also be noted, that currently deployed analog VHF voice radios support direct voice communication between aircraft, making a similar use case for digital voice plausible.¶

LDACS A/A is currently not part of the standardization process and will not be covered within this document. However, it is planned that LDACS A/A will be rolled out after the initial deployment of LDACS A/G, then being seamlessly integrated in the existing LDACS ground-based system.¶

5.2.3. Flight Guidance

The FCI (and therefore LDACS) is used to provide flight guidance. This is realized using three applications:¶

1.: Context Management (CM): The CM application manages the automatic logical connection to the ATC center currently responsible to guide the aircraft. Currently, this is done by the air crew manually changing VHF voice frequencies manually according to the progress of the flight. The CM application automatically sets up equivalent sessions.¶
2.: Controller Pilot Data Link Communications (CPDLC): The CPDLC application provides the air crew with the ability to exchange data messages similar to text messages with the currently responsible ATC center. The CPDLC application takes over most of the communication currently performed over VHF voice and enables new services that do not lend themselves to voice communication (i.e., trajectory negotiation).¶
3.: Automatic Dependent Surveillance - Contract (ADS-C): ADS-C reports the position of the aircraft to the currently active ATC center. Reporting is bound to "contracts", i.e., pre-defined events related to the progress of the flight (i.e., the trajectory). ADS-C and CPDLC are the primary applications used for implementing in-flight trajectory management.¶

CM, CPDLC, and ADS-C are available on legacy datalinks, but are not widely deployed and with limited functionality.¶

Further ATC applications may be ported to use the FCI or LDACS as well. A notable application is GBAS for secure, automated landings: The Global Navigation Satellite System (GNSS) based GBAS is used to improve the accuracy of GNSS to allow GNSS based instrument landings. This is realized by sending GNSS correction data (e.g., compensating ionospheric errors in the GNSS signal) to the aircraft's GNSS receiver via a separate data link. Currently, the VDB data link is used. VDB is a narrowband single-purpose datalink without advanced security only used to transmit GBAS correction data. This makes VDB a natural candidate for replacement by LDACS [MAE20211].¶

5.2.4. Business Communications of Airlines

In addition to air traffic services, AOC services are transmitted over LDACS. AOC is a generic term referring to the business communication of airlines, between the airlines and service partners on the ground and their own aircraft in the air. Regulatory-wise, this is considered related to safety and regularity of flight and may therefore, be transmitted over LDACS. AOC communication is considered the main business case for LDACS communications service providers since modern aircraft generate significant amounts of data (e.g., engine maintenance data).¶

Beyond communications, radio signals can always also be used for navigation. This fact is used for the LDACS navigation concept.¶

For future aeronautical navigation, ICAO recommends the further development of GNSS based technologies as primary means for navigation. Due to the large separation between navigational satellites and aircraft, the power of the GNSS signals received by the aircraft is, however, very low. As a result, GNSS disruptions might occasionally occur due to unintentional interference, or intentional jamming. Yet the navigation services must be available with sufficient performance for all phases of flight. Therefore, during GNSS outages, or blockages, an alternative solution is needed. This is commonly referred to as Alternative Positioning, Navigation, and Timing (APNT).¶

One such APNT solution is based on exploiting the built-in navigation capabilities of LDACS operation. That is, the normal operation of LDACS for ATC and AOC communications would also directly enable the aircraft to navigate and obtain a reliable timing reference from the LDACS GSs. Current cell planning for Europe shows 84 LDACS cells to be sufficient [MOST2018] to cover the continent at sufficient service level. If more than three Ground Stations (GS) are visible by the aircraft, via knowing the exact positions of these and having a good channel estimation (which LDACS does due to numerous works mapping the L-band channel characteristics [SCHN2018] ) it is possible to calculate the position of the aircraft via measuring signal propagation times to each GS. In flight trials in 2019 with one aircraft (and airborne radio inside it) and just four GS, navigation feasibility was demonstrated within the footprint of all four GS with a 95th percentile position-domain error of 171.1m [OSE2019] [BEL2021] [MAE20211]. As such, LDACS can be used independently of GNSS as a navigation alternative. Positioning errors will decrease markedly as more GSes are deployed. [OSE2019] [BEL2021] [MAE20211]¶

LDACS navigation has already been demonstrated in practice in two flight measurement campaigns [SHU2013] [BEL2021] [MAE20211].¶

6. Requirements

The requirements for LDACS are mostly defined by its application area: Communications related to safety and regularity of flight.¶

A particularity of the current aeronautical communication landscape is that it is heavily regulated. Aeronautical data links (for applications related to safety and regularity of flight) may only use spectrum licensed to aviation and data links endorsed by ICAO. Nation states can change this locally; however, due to the global scale of the air transportation system, adherence to these practices is to be expected.¶

Aeronautical data links for the ATN are therefore expected to remain in service for decades. The VDLm2 data link currently used for digital terrestrial internetworking was developed in the 1990s (the use of the Open Systems Interconnection (OSI) stack indicates that as well). VDLm2 is expected to be used at least for several decades to come. In this respect aeronautical communications (for applications related to safety and regularity of flight) is more comparable to industrial applications than to the open Internet.¶

Internetwork technology is already installed in current aircraft. Current ATS applications use either Aircraft Communications Addressing and Reporting System (ACARS) or the OSI stack. The objective of the development effort of LDACS, as part of the FCI, is to replace legacy OSI stack and proprietary ACARS internetwork technologies with industry standard IP technology. It is anticipated that the use of Commercial Off-The-Shelf (COTS) IP technology mostly applies to the ground network. The avionics networks on the aircraft will likely be heavily modified versions of Ethernet or proprietary.¶

AOC applications currently mostly use the same stack (although some applications, like the graphical weather service may use the commercial passenger network). This creates capacity problems (resulting in excessive amounts of timeouts) since the underlying terrestrial data links do not provide sufficient bandwidth (i.e., with VDLm2 currently in the order of 10 kbit/s). The use of non- aviation specific data links is considered a security problem. Ideally the aeronautical IP internetwork, hence the ATN over which only communications related to safety and regularity of flight is handled, and the Internet should be completely separated at Layer 3.¶

The objective of LDACS is to provide a next generation terrestrial data link designed to support IP addressing and provide much higher bandwidth to avoid the currently experienced operational problems.¶

The requirement for LDACS is therefore to provide a terrestrial high-throughput data link for IP internetworking in the aircraft.¶

In order to fulfil the above requirement LDACS needs to be interoperable with IP (and IP-based services like Voice-over-IP) at the gateway connecting the LDACS network to other aeronautical ground networks (i.e., the ATN). On the avionics side, in the aircraft, aviation specific solutions are to be expected.¶

In addition to these functional requirements, LDACS and its IP stack need to fulfil the requirements defined in RTCA DO-350A/EUROCAE ED-228A [DO350A]. This document defines continuity, availability, and integrity requirements at different scopes for each air traffic management application (CPDLC, CM, and ADS-C). The scope most relevant to IP over LDACS is the Communications Service Provider (CSP) scope.¶

Continuity, availability, and integrity requirements are defined in [DO350A] volume 1 Table 5-14, and Table 6-13. Appendix A presents the required information.¶

In a similar vein, requirements to fault management are defined in the same tables.¶

7. Characteristics

LDACS will become one of several wireless access networks connecting aircraft to the ATN implemented by the FCI.¶

The current LDACS design is focused on the specification of layer one and two. However, for the purpose of this work, only layer two details are discussed here.¶

Achieving the stringent continuity, availability, and integrity requirements defined in [DO350A] will require the specification of layer 3 and above mechanisms (e.g., reliable crossover at the IP layer). Fault management mechanisms are similarly unspecified as of November 2022. Current regulatory documents do not fully specify the above mechanism yet. However, a short overview of the current state shall be given throughout each section here.¶

7.1. LDACS Access Network

An LDACS access network contains an Access Router (AC-R) and several GS, each of them providing one LDACS radio cell.¶

User plane interconnection to the ATN is facilitated by the AC-R peering with an A/G Router connected to the ATN.¶

The internal control plane of an LDACS access network interconnects the GSs. An LDACS access network is illustrated in Figure 1.¶



wireless                user
link                    plane
  AS-------------GS---------------AC-R---A/G-----ATN
    ..............                 |   Router
       control   .                 |
       plane     .                 |
                 .                 |
                 GS----------------|
                 .                 |
                 .                 |
                 GS----------------+

Figure 1: LDACS access network with three GSs and one AS. dashes denotes the user plane and points the control plane

7.2. Topology

LDACS is a cellular point-to-multipoint system. It assumes a star-topology in each cell where Aircraft Stations (AS) belonging to aircraft within a certain volume of space (the LDACS cell) are connected to the controlling GS. The LDACS GS is a centralized instance that controls LDACS A/G communications within its cell. The LDACS GS can simultaneously support multiple bidirectional communications to the ASs under its control. LDACS's GSs themselves are connected to each other and the AC-R.¶

Prior to utilizing the system an aircraft has to register with the controlling GS to establish dedicated logical channels for user and control data. Control channels have statically allocated resources, while user channels have dynamically assigned resources according to the current demand. Logical channels exist only between the GS and the AS.¶

7.3. LDACS Protocol Stack

The protocol stack of LDACS is implemented in the AS and GS: It consists of the Physical Layer (PHY) with five major, functional blocks above it. Four are placed in the Data Link Layer (DLL) of the AS and GS: (1) Medium Access Control (MAC) Layer, (2) Voice Interface (VI), (3) Data Link Service (DLS), and (4) LDACS Management Entity (LME). The fifth entity resides within the sub-network layer: (5) the Sub-Network Protocol (SNP). The LDACS radio is externally connected to a voice unit, radio control unit, and via the AC-R to the ATN network.¶

LDACS is considered an ATN/IPS radio access technology, from the view of ICAO's regulatory framework. Hence, the interface between ATN and LDACS must be IPv6 based, as regulatory documents, such as ICAO Doc 9896 [ICAO2015] and DO-379 [RTCA2019] clearly foresee that. The translation between IPv6 layer and SNP layer is currently the subject of ongoing standardization efforts and at the time of writing not finished yet.¶

Figure 2 shows the protocol stack of LDACS as implemented in the AS and GS. Acronyms used here are introduced throughout the upcoming sections.¶



                   IPv6                   Network Layer
                     |
Airborne Voice       |
Interface (AVI)/     |               Radio Control Unit (RCU)
Voice Unit (VU)      |
   |                 |
   |      +------------------+  +----+
   |      |        SNP       |--|    |   Sub-Network
   |      |                  |  |    |   Layer
   |      +------------------+  |    |
   |                |           | LME|
+-----+   +------------------+  |    |
| VI  |   |        DLS       |  |    |   LLC Layer
+-----+   +------------------+  +----+
   |                |             |
  DCH              DCH         DCCH/CCCH
                    |          RACH/BCCH
                    |             |
+-------------------------------------+
|                  MAC                |   Medium Access
|                                     |   Layer
+-------------------------------------+
                    |
+-------------------------------------+
|                  PHY                |   Physical Layer
+-------------------------------------+
                    |
                    |
                  ((*))
                  FL/RL              radio channels
                                    separated by FDD

Figure 2: LDACS protocol stack in AS and GS

7.3.1. LDACS Physical Layer

The physical layer provides the means to transfer data over the radio channel. The LDACS GS supports bidirectional links to multiple aircraft under its control. The FL direction at the G2A connection and the RL direction at the A2G connection are separated by Frequency Division Duplex (FDD). FL and RL use a 500 kHz channel each. The GS transmits a continuous stream of Orthogonal Frequency-Division Multiplexing Access (OFDM) symbols on the FL. In the RL different aircraft are separated in time and frequency using Orthogonal Frequency-Division Multiple Access (OFDMA). Aircraft thus transmit discontinuously on the RL via short radio bursts sent in precisely defined transmission opportunities allocated by the GS.¶

7.3.2. LDACS Data Link Layer

The data-link layer provides the necessary protocols to facilitate concurrent and reliable data transfer for multiple users. The LDACS data link layer is organized in two sub-layers: The medium access sub-layer and the Logical Link Control (LLC) sub-layer. The medium access sub-layer manages the organization of transmission opportunities in slots of time and frequency. The LLC sub-layer provides acknowledged point-to-point logical channels between the aircraft and the GS using an Automatic Repeat reQuest (ARQ) protocol. LDACS also supports unacknowledged point-to-point channels and G2A Broadcast transmission.¶

7.3.2.1. Medium Access Control (MAC) Services

The MAC time framing service provides the frame structure necessary to realize slot-based time-division multiplex-access on the physical link. It provides the functions for the synchronization of the MAC framing structure and the PHY Layer framing. The MAC time framing provides a dedicated time slot for each logical channel.¶

The MAC sub-layer offers access to the physical channel to its service users. Channel access is provided through transparent logical channels. The MAC sub-layer maps logical channels onto the appropriate slots and manages the access to these channels. Logical channels are used as interface between the MAC and LLC sub-layers.¶

7.3.2.2. Data Link Service (DLS) Services

The DLS provides acknowledged and unacknowledged (including broadcast and packet mode voice) bidirectional exchange of user data. If user data is transmitted using the acknowledged DLS, the sending DLS entity will wait for an acknowledgement from the receiver. If no acknowledgement is received within a specified time frame, the sender may automatically try to retransmit its data. However, after a certain number of failed retries, the sender will suspend further retransmission attempts and inform its client of the failure.¶

The DLS uses the logical channels provided by the MAC:¶

1.: A GS announces its existence and access parameters in the Broadcast Channel (BCCH).¶
2.: The Random-Access Channel (RACH) enables AS to request access to an LDACS cell.¶
3.: In the FL the Common Control Channel (CCCH) is used by the GS to grant access to data channel resources.¶
4.: The reverse direction is covered by the RL, where ASs need to request resources before sending. This happens via the Dedicated Control Channel (DCCH).¶
5.: User data itself is communicated in the Data Channel (DCH) on the FL and RL.¶

Access to the FL and RL data channel is granted by the scheduling mechanism implemented in the LME discussed below.¶

7.3.2.3. Voice Interface (VI) Services

The VI provides support for virtual voice circuits. Voice circuits may either be set-up permanently by the GS (e.g., to emulate voice party line) or may be created on demand.¶

7.3.2.4. LDACS Management Entity (LME) Services

The mobility management service in the LME provides support for registration and de-registration (cell entry and cell exit), scanning RF channels of neighboring cells and handover between cells. In addition, it manages the addressing of aircraft within cells.¶

The resource management service provides link maintenance (power, frequency and time adjustments), support for adaptive coding and modulation, and resource allocation.¶

The resource management service accepts resource requests from/for different AS and issues resource allocations accordingly. While the scheduling algorithm is not specified and a point of possible vendor differentiation, it is subject to the following requirements:¶

1.: Resource scheduling must provide channel access according to the priority of the request¶
2.: Resource scheduling must support "one-time" requests.¶
3.: Resource scheduling must support "permanent" requests that reserve a resource until the request is canceled e.g. for digital voice circuits.¶

7.3.3. LDACS Sub-Network Layer and Protocol Services

Lastly, the SNP layer of LDACS directly interacts with IPv6 traffic. Incoming ATN/IPS IPv6 packets are forwarded over LDACS from and to the aircraft. The final IP addressing structure in an LDACS subnet still needs to be defined; however, the current layout is considered to consist of the five network segments: Air Core Net, Air Management Net, Ground Core Net, Ground Management Net, Ground Net. Any protocols that the ATN/IPS [ICAO2015] defines as mandatory will reach the aircraft, however listing these here is out of scope. For more information on the technicalities of the above ATN/IPS layer, please refer to [ICAO2015] [RTCA2019] [ARI2021].¶

The DLS provides functions required for the transfer of user plane data and control plane data over the LDACS access network. The security service provides functions for secure user data communication over the LDACS access network. Note that the SNP security service applies cryptographic measures as configured by the GS.¶

7.4. LDACS Mobility

LDACS supports layer 2 handovers to different LDACS cells. Handovers may be initiated by the aircraft (break-before-make) or by the GS (make-before-break). Make-before-break handovers are only supported between GSs connected to each other, usually GS operated by the same service provider.¶

When a handover between AS and two interconnected GS takes place, it can be triggered by AS or GS. Once that is done, new security information is exchanged between AS, GS1 and GS2, before the "old" connection is terminated between AS and GS1 and a "new" connection is set up between AS and GS2. As a last step, accumulated user-data at GS1 is forwarded to GS2 via a ground connection, before that is sent via GS2 to the AS. While some information for handover is transmitted in the LDACS DCH, the information remains in the "control-plane" part of LDACS and is exchanged between LMEs in AS, GS1 and GS2. As such, local mobility takes place entirely within the LDACS network, utilizing the PMIPv6 protocol [RFC5213]. The use of PMIPv6 is currently not mandated by standardization, and may be vendor-specific. External handovers between non-connected LDACS access networks or different aeronautical data links are handled by the FCI multi-link concept.¶

External handovers between non-connected LDACS access networks or different aeronautical data links are handled by the FCI multi- link concept.¶

7.5. LDACS Management - Interfaces and Protocols

LDACS management interfaces and protocols are currently not be mandated by standardization. The implementations currently available use SNMP for management and Radius for AAA. Link state (link up, link down) is reported using the ATN/IPS Aircraft Protocol (AIAP) mandated by ICAO WG-I for multi-link.¶

8. Reliability and Availability

8.1. Below Layer 1

Below Layer 2, aeronautics usually relies on hardware redundancy. To protect availability of the LDACS link, an aircraft equipped with LDACS will have access to two L-band antennae with triple redundant radio systems as required for any safety relevant aeronautical systems by ICAO.¶

8.2. Layer 1 and 2

LDACS has been designed with applications related to the safety and regularity of flight in mind. It has therefore been designed as a deterministic wireless data link (as far as this is possible).¶

Based on channel measurements of the L-band channel LDACS was designed from the PHY layer up with robustness in mind. Channel measurements of the L-band channel [SCH2016] confirmed LDACS to be well adapted to its channel.¶

In order to maximize the capacity per channel and to optimally use the available spectrum, LDACS was designed as an OFDM-based FDD system, supporting simultaneous transmissions in FL in the G2A connection and RL in the A2G connection. The legacy systems already deployed in the L-band limit the bandwidth of both channels to approximately 500 kHz.¶

The LDACS physical layer design includes propagation guard times sufficient for operation at a maximum distance of 200 nautical miles from the GS. In actual deployment, LDACS can be configured for any range up to this maximum range.¶

The LDACS physical layer supports adaptive coding and modulation for user data. Control data is always encoded with the most robust coding and modulation (FL: Quadrature Phase-Shift Keying (QPSK), coding rate 1/2, RL: QPSK, coding rate 1/3).¶

LDACS medium access layer on top of the physical layer uses a static frame structure to support deterministic timer management. As shown in Figure 3 and Figure 4, LDACS framing structure is based on Super- Frames (SF) of 240ms duration corresponding to 2000 OFDM symbols. OFDM symbol time is 120 microseconds, sampling time 1.6 microseconds and a guard time of 4.8 microseconds. The structure of a SF is depicted in Figure 3 along with its structure and timings of each part. FL and RL boundaries are aligned in time (from the GS perspective) allowing for deterministic slots for control and data channels. This initial AS time synchronization and time synchronization maintenance is based on observing the synchronization symbol pairs that repetitively occur within the FL stream, being sent by the controlling GS [GRA2020]. As already mentioned, LDACS data transmission is split into user-data (DCH) and control (BCCH, CCCH in FL; RACH, DCCH in RL) as depicted with corresponding timings in Figure 4.¶


^
|     +--------+------------+------------+------------+------------+
|  FL |  BCCH  |     MF     |     MF     |     MF     |     MF     |
|     | 6.72ms |   58.32ms  |   58.32ms  |   58.32ms  |   58.32ms  |
F     +--------+------------+------------+------------+------------+
r     <----------------- Super-Frame (SF) - 240ms ----------------->
e
q     +--------+------------+------------+------------+------------+
u  RL |  RACH  |     MF     |     MF     |     MF     |     MF     |
e     | 6.72ms |   58.32ms  |   58.32ms  |   58.32ms  |   58.32ms  |
n     +--------+------------+------------+------------+------------+
c     <----------------- Super-Frame (SF) - 240ms ----------------->
y
------------------------------ Time ------------------------------->
|

Figure 3: SF structure for LDACS


^
|     +-------------+----------------+-----------------+
|  FL |     DCH     |     CCCH       |      DCH        |
|     |   25.92ms   | 2.16 - 17.28ms | 15.12 - 30.24ms |
F     +-------------+----------------+-----------------+
r     <----------- Multi-Frame (MF) - 58.32ms --------->
e
q     +--------------+---------------------------------+
u  RL |    DCCH      |                DCH              |
e     | 2.8 - 24.4ms |           33.84 - 55.44ms       |
n     +--------------+---------------------------------+
c     <----------- Multi-Frame (MF) - 58.32ms --------->
y
----------------------------- Time -------------------->
|

Figure 4: MF structure for LDACS

LDACS cell entry is conducted with an initial control message exchange via the RACH and the BCCH.¶

After cell entry, LDACS medium access is always under the control of the GS of a radio cell. Any medium access for the transmission of user data on a DCH has to be requested with a resource request message stating the requested amount of resources and class of service. The GS performs resource scheduling on the basis of these requests and grants resources with resource allocation messages. Resource request and allocation messages are exchanged over dedicated contention-free control channels (DCCH and CCCH).¶

The purpose of quality-of-service in LDACS medium access is to provide prioritized medium access at the bottleneck (the wireless link). Signaling of higher layer quality-of-service requests to LDACS is implemented on the basis of Differentiated Services-(DiffServ) classes CS01 (lowest priority) to CS07 (highest priority).¶

In addition to having full control over resource scheduling, the GS can send forced handover commands for off-loading or channel management, e.g., when the signal quality declines and a more suitable GS is in the AS's reach. With robust resource management of the capacities of the radio channel, reliability and robustness measures are therefore also anchored in the LME.¶

In addition to radio resource management, the LDACS control channels are also used to send keep-alive messages, when they are not otherwise used. Since the framing of the control channels is deterministic, missing keep-alive messages can thus be immediately detected. This information is made available to the multilink protocols for fault management.¶

The protocol used to communicate faults is not defined in the LDACS specification. It is assumed that vendors would use industry standard protocols like the Simple Network Management Protocol or the Network Configuration Protocol, where security permits.¶

The LDACS data link layer protocol, running on top of the medium access sub-layer, uses ARQ to provide reliable data transmission on the data channel.¶

It employs selective repeat ARQ with transparent fragmentation and reassembly to the resource allocation size to minimize latency and overhead without losing reliability. It ensures correct order of packet delivery without duplicates. In case of transmission errors, it identifies lost fragments with deterministic timers synced to the medium access frame structure and initiates retransmission.¶

8.3. Beyond Layer 2

LDACS availability can be increased by appropriately deploying LDACS infrastructure: This means proliferating the number of terrestrial ground stations. However, there are four aspects that need to be taken into consideration: (1) scarcity of aeronautical spectrum for data link communication (in the case of LDACS: tens of MHz in the L-band), (2) an increase in the amount of ground stations also increases the individual bandwidth for aircraft in the cell, as fewer aircraft have to share the spectrum, (3) to cover worldwide terrestrial ATM via LDACS is also a question of cost and the possible reuse of spectrum which makes it not always possible to decrease cell sizes and (4) the Distance Measuring Equipment (DME) is the primary user of the aeronautical L-band, which means any LDACS deployment has to take DME frequency planning into account.¶

While aspect (2) provides a good reason, alongside increasing redundancy, for smaller cells than the maximum range LDACS was developed for (200 Nautical Miles (NM)), the other three need to be respected when doing so. There are preliminary works on LDACS cell planning, such as [MOST2018], where the authors reach the conclusion that 84 LDACS cells in Europe would be sufficient to serve European air traffic for the next 20 years.¶

For redundancy reasons, the aeronautical community has decided not to rely on a single communication system or frequency band. It is envisioned to have multiple independent data link technologies in the aircraft (e.g., terrestrial and satellite communications) in addition to legacy VHF voice.¶

However, as of now, no reliability and availability mechanisms that could utilize the multilink architecture, have been specified on Layer 3 and above. Even if LDACS has been designed for reliability, the wireless medium presents significant challenges to achieve deterministic properties such as low packet error rate, bounded consecutive losses, and bounded latency. Support for high reliability and availability for IP connectivity over LDACS is certainly highly desirable but needs to be adapted to the specific use case.¶

9. Security

The goal of this Section is to inform the reader about the state of security in aeronautical communications, state security considerations applicable for all ATN/IPS traffic and to provide an overview of the LDACS link-layer security capabilities.¶

9.1. Security in Wireless Digital Aeronautical Communications

Aviation will require secure exchanges of data and voice messages for managing the air traffic flow safely through the airspaces all over the world. Historically Communication Navigation Surveillance (CNS) wireless communications technology emerged from the military and a threat landscape where inferior technological and financial capabilities of adversaries were assumed [STR2016]. The main communications method for ATC today is still an open analogue voice broadcast within the aeronautical VHF band. Currently, information security is mainly procedural, based by using well-trained personnel and proven communications procedures. This communication method has been in service since 1948. However, since the emergence of civil aeronautical CNS applications in the 70s, and today, the world has changed.¶

CCivil applications have significant lower spectrum available than military applications. This means several military defense mechanisms, such as frequency hopping or pilot symbol scrambling and, thus, a defense-in-depth approach starting at the physical layer, is infeasible for civil systems. With the rise of cheap Software Defined Radios (SDR), the previously existing financial barrier is almost gone and open source projects such as GNU radio [GNU2021] allow a new type of unsophisticated listeners and possible attackers.¶

Most CNS technology developed in ICAO relies on open standards, thus syntax and semantics of wireless digital aeronautical communications should be expected to be common knowledge for attackers. With increased digitization and automation of civil aviation, the human as control instance, is being taken gradually out of the loop. Autonomous transport drones or single piloted aircraft demonstrate this trend. However, without profound cybersecurity measures such as authenticity and integrity checks of messages in-transit on the wireless link or mutual entity authentication, this lack of a control instance can prove disastrous. Thus, future digital communications will need additional embedded security features to fulfill modern information security requirements like authentication and integrity. These security features require sufficient bandwidth which is beyond the capabilities of currently deployed VHF narrowband communications systems. For voice and data communications, sufficient data throughput capability is needed to support the security functions while not degrading performance. LDACS is a data link technology with sufficient bandwidth to incorporate security without losing too much user data throughput.¶

9.2. Security in Depth

ICAO Doc 9896 foresees transport layer security [ICAO2015] for all aeronautical data transmitted via the ATN/IPS, as described in ARINC P858 [ARI2021]. This is realized via Datagram Transport Layer Security (DTLS) 1.3 [RFC9147].¶

LDACS also needs to comply with in-depth security requirements, stated in ARINC 858, for the radio access technologies transporting ATN/IPS data. These requirements imply that LDACS must provide layer 2 security in addition to any higher layer mechanisms. Specifically, ARINC 858 states that [datalinks within the FCI need to provide] "a secure channel between the airborne radio systems and the peer radio access endpoints on the ground [...] to ensure authentication and integrity of air-ground message exchanges in support of an overall defense-in-depth security strategy." [ARI2021]¶

9.3. LDACS Security Requirements

Overall, cybersecurity for CNS technology shall protect the following business goals [MAE20181]:¶

1.: Safety: The system must sufficiently mitigate attacks, which contribute to safety hazards.¶
2.: Flight regularity: The system must sufficiently mitigate attacks, which contribute to delays, diversions, or cancellations of flights.¶
3.: Protection of business interests: The system must sufficiently mitigate attacks which result in financial loss, reputation damage, disclosure of sensitive proprietary information, or disclosure of personal information.¶

To further analyze assets and derive threats and thus protection scenarios several threat-and risk analyses were performed for LDACS [MAE20181] , [MAE20191]. These results allowed the derivation of security scope and objectives from the requirements and the conducted threat-and risk analysis. Note, IPv6 security considerations are briefly discussed in Section 9.7 while a summary of security requirements for link-layer candidates in the ATN/IPS is given in [ARI2021], which states: "Since the communication radios connect to local airborne networks in the aircraft control domain, [...] the airborne radio systems represent the first point of entry for an external threat to the aircraft. Consequently, a secure channel between the airborne radio systems and the peer radio access endpoints on the ground is necessary to ensure authentication and integrity of air-ground message exchanges in support of an overall defense-in-depth security strategy".¶

9.4. LDACS Security Objectives

Security considerations for LDACS are defined by the official SARPS document by ICAO [ICAO2022]:¶

1.: LDACS shall provide a capability to protect the availability and continuity of the system.¶
2.: LDACS shall provide a capability including cryptographic mechanisms to protect the integrity of messages in transit.¶
3.: LDACS shall provide a capability to ensure the authenticity of messages in transit.¶
4.: LDACS should provide a capability for nonrepudiation of origin for messages in transit.¶
5.: LDACS should provide a capability to protect the confidentiality of messages in transit.¶
6.: LDACS shall provide an authentication capability.¶
7.: LDACS shall provide a capability to authorize the permitted actions of users of the system and to deny actions that are not explicitly authorized.¶
8.: If LDACS provides interfaces to multiple domains, LDACS shall provide capability to prevent the propagation of intrusions within LDACS domains and towards external domains.¶

Work in 2022 includes a change request for these SARPS aims to limit the "non-repudiation of origin of messages in transit" requirement only to the authentication and key establishment messages at the beginning of every session.¶

9.5. LDACS Security Functions

These objectives were used to derive several security functions for LDACS required to be integrated in the LDACS cybersecurity architecture: Identification, Authentication, Authorization, Confidentiality, System Integrity, Data Integrity, Robustness, Reliability, Availability, and Key and Trust Management. Several works investigated possible measures to implement these security functions [BIL2017], [MAE20181], [MAE20191].¶

9.6. LDACS Security Architecture

The requirements lead to a LDACS security model, including different entities for identification, authentication and authorization purposes, ensuring integrity, authenticity and confidentiality of data. A draft of the cybersecurity architecture of LDACS can be found in [ICAO2022] and [MAE20182] and respective updates in [MAE20191], [MAE20192], [MAE2020], [MAE2021].¶

9.6.1. Entities

A simplified LDACS architectural model requires the following entities: Network operators such as the Societe Internationale de Telecommunications Aeronautiques (SITA) [SIT2020] and ARINC [ARI2020] are providing access to the ground IPS network via an A/G LDACS router. This router is attached to an internal LDACS access network, which connects via further access routers to the different LDACS cell ranges, each controlled by a GS (serving one LDACS cell), with several interconnected GS spanning a local LDACS access network. Via the A/G wireless LDACS data link AS the aircraft is connected to the ground network and via the aircraft's VI and aircraft's network interface, aircraft's data can be sent via the AS back to the GS, then to the LDACS local access network, access routers, LDACS access network, A/G LDACS router and finally to the ground IPS network [ICAO2015].¶

9.6.2. Entity Identification

LDACS needs specific identities for the AS, the GS, and the network operator. The aircraft itself can be identified using the 24-bit ICAO identifier of an aircraft [ICAO2022], the call sign of that aircraft or the recently founded privacy ICAO address of the Federal Aviation Administration (FAA) program with the same name [FAA2020]. It is conceivable that the LDACS AS will use a combination of aircraft identification, radio component identification and even operator feature identification to create a unique AS LDACS identification tag. Similar to a 4G's eNodeB serving network identification tag, a GS could be identified using a similar field. The identification of the network operator is again similar to 4G (e.g., E-Plus, AT&T, and TELUS), in the way that the aeronautical network operators are listed (e.g., ARINC [ARI2020] and SITA [SIT2020]).¶

9.6.3. Entity Authentication and Key Establishment

In order to anchor trust within the system, all LDACS entities connected to the ground IPS network will be rooted in an LDACS specific chain-of-trust and PKI solution, quite similar to AeroMACS's approach [CRO2016]. These certificates, residing at the entities and incorporated in the LDACS PKI, providing proof the ownership of their respective public key, include information about the identity of the owner and the digital signature of the entity that has verified the certificate's content. First, all ground infrastructures must mutually authenticate to each other, negotiate and derive keys and, thus, secure all ground connections. How this process is handled in detail is still an ongoing discussion. However, established methods to secure user plane by IPSec [RFC4301] and IKEv2 [RFC7296] or the application layer via TLS 1.3 [RFC8446] are conceivable. The LDACS PKI with its chain-of-trust approach, digital certificates and public entity keys lay the groundwork for this step. In a second step, the AS with the LDACS radio aboard, approaches an LDACS cell and performs a cell-attachment procedure with the corresponding GS. This procedure consists of (1) the basic cell entry [GRA2020] and (2) a Mutual Authentication and Key Establishment (MAKE) procedure [MAE2021].¶

Note that LDACS will foresee multiple security levels. To address the issue of the long service life of LDACS (i.e., possibly >30 years) and the security of current pre-quantum cryptography, these security levels include pre- and post-quantum cryptographic solutions. Limiting security data on the LDACS datalink as much as possible, to reserve as much space for actual user data transmission, is key in the LDACS security architecture, this is also reflected in the underlying cryptography: Pre-quantum solutions will rely on elliptic curves [NIST2013], while post-quantum solutions consider Falcon [SON2021] [MAE2021] or similar lightweight PQC signature schemes, and CRYSTALS-KYBER or SABER as key establishment options [AVA2021] [ROY2020].¶

9.6.4. Message-in-transit Confidentiality, Integrity and Authenticity

The key material from the previous step can then be used to protect LDACS Layer 2 communications via applying encryption and integrity protection measures on the SNP layer of the LDACS protocol stack. As LDACS transports AOC and ATS data, the integrity of that data is most important, while confidentiality only needs to be applied to AOC data to protect business interests [ICAO2022]. This possibility of providing low layered confidentiality and integrity protection ensures a secure delivery of user data over the wireless link. Furthermore, it ensures integrity protection of LDACS control data.¶

9.7. Considerations on LDACS Security Impact on IPv6 Operational Security

In this part, considerations on IPv6 operational security in [RFC9099] and interrelations with the LDACS security additions are compared and evaluated to identify further protection demands. As IPv6 heavily relies on the Neighbor Discovery Protocol (NDP) [RFC4861], integrity and authenticity protection on the link-layer, as provided by LDACS, already help mitigate spoofing and redirection attacks. However, to also mitigate the threat of remote DDoS attacks, neighbor solicitation rate-limiting is recommended by RFC 9099. To prevent the threat of (D)DoS attacks in general on the LDACS access network, rate-limiting needs to be performed on each network node in the LDACS access network. One approach is to filter for the total amount of possible LDACS AS-GS traffic per cell - i.e., of up to 1.4 Mbps user-data per cell and up to the amount of GS per service provider network times 1.4 Mbps.¶

13. Informative References

[RFC4301]: Kent, S. and K. Seo, "Security Architecture for the Internet Protocol", RFC 4301, DOI 10.17487/RFC4301, December 2005, <https://www.rfc-editor.org/info/rfc4301>.
[RFC4861]: Narten, T., Nordmark, E., Simpson, W., and H. Soliman, "Neighbor Discovery for IP version 6 (IPv6)", RFC 4861, DOI 10.17487/RFC4861, September 2007, <https://www.rfc-editor.org/info/rfc4861>.
[RFC5213]: Gundavelli, S., Ed., Leung, K., Devarapalli, V., Chowdhury, K., and B. Patil, "Proxy Mobile IPv6", RFC 5213, DOI 10.17487/RFC5213, August 2008, <https://www.rfc-editor.org/info/rfc5213>.
[RFC5795]: Sandlund, K., Pelletier, G., and L. Jonsson, "The RObust Header Compression (ROHC) Framework", RFC 5795, DOI 10.17487/RFC5795, March 2010, <https://www.rfc-editor.org/info/rfc5795>.
[RFC7296]: Kaufman, C., Hoffman, P., Nir, Y., Eronen, P., and T. Kivinen, "Internet Key Exchange Protocol Version 2 (IKEv2)", STD 79, RFC 7296, DOI 10.17487/RFC7296, October 2014, <https://www.rfc-editor.org/info/rfc7296>.
[RFC8200]: Deering, S. and R. Hinden, "Internet Protocol, Version 6 (IPv6) Specification", STD 86, RFC 8200, DOI 10.17487/RFC8200, July 2017, <https://www.rfc-editor.org/info/rfc8200>.
[RFC8446]: Rescorla, E., "The Transport Layer Security (TLS) Protocol Version 1.3", RFC 8446, DOI 10.17487/RFC8446, August 2018, <https://www.rfc-editor.org/info/rfc8446>.
[RFC9099]: Vyncke, É., Chittimaneni, K., Kaeo, M., and E. Rey, "Operational Security Considerations for IPv6 Networks", RFC 9099, DOI 10.17487/RFC9099, August 2021, <https://www.rfc-editor.org/info/rfc9099>.
[RFC9147]: Rescorla, E., Tschofenig, H., and N. Modadugu, "The Datagram Transport Layer Security (DTLS) Protocol Version 1.3", RFC 9147, DOI 10.17487/RFC9147, April 2022, <https://www.rfc-editor.org/info/rfc9147>.
[GRA2020]: Gräupl, T., Rihacek, C., and B. Haindl, "LDACS A/G Specification", SESAR2020 PJ14-02-01 D3.3.030 , 2020, <https://www.ldacs.com/wp-content/uploads/2013/12/SESAR2020_PJ14-W2-60_D3_1_210_Initial_LDACS_AG_Specification_00_01_00-1_0_updated.pdf>.
[ARI2021]: ARINC, "Internet Protocol Suite (IPS) For Aeronautical Safety Services Part 1- Airborne IP System Technical Requirements, ARINC SPECIFICATION 858 P1", June 2021, <https://standards.globalspec.com/std/14391274/858p1>.
[EURO2019]: European Organization for Civil Aviation Equipment (EUROCAE), "Technical Standard of Aviation Profiles for ATN/IPS, ED-262", September 2019, <https://eshop.eurocae.net/eurocae-documents-and-reports/ed-262/>.
[ICAO2015]: International Civil Aviation Organization (ICAO), "Manual on the Aeronautical Telecommunication Network (ATN) using Internet Protocol Suite (IPS) Standards and Protocols, Doc 9896", January 2015, <https://standards.globalspec.com/std/10026940/icao-9896>.
[RTCA2019]: Radio Technical Commission for Aeronautics (RTCA), "Internet Protocol Suite Profiles, DO-379", September 2019, <https://www.rtca.org/products/do-379/>.
[SCH2016]: Schneckenburger, N., Jost, T., Shutin, D., Walter, M., Thiasiriphet, T., Schnell, M., and U.C. Fiebig, "Measurement of the L-band Air-to-Ground Channel for Positioning Applications", IEEE Transactions on Aerospace and Electronic Systems, 52(5), pp.2281-229 , 2016.
[OSE2019]: Osechas, O., Narayanan, S., Crespillo, O.G., Zampieri, G., Battista, G., Kumar, R., Schneckenburger, N., Lay, E., Belabbas, B., and M. Meurer, "Feasibility Demonstration of Terrestrial RNP with LDACS", 32nd International Technical Meeting of the Satellite Division of The Institute of Navigation, pp.1-12 , 2019.
[SCHN2018]: Schneckenburger, N., "A Wide-Band Air-Ground Channel Mode", Dissertation, Technische Universitaet Ilmenau, Ilmenau, Germany , 2018.
[MOST2018]: Mostafa, M., Bellido-Manganell, M.A.., and T. Gräupl, "Feasibility of Cell Planning for the L-Band Digital Aeronautical Communications System Under the Constraint of Secondary Spectrum Usage", IEEE Transactions on Vehicular Technology, vol. 67, no. 10, pp. 9721-9733 , 2018.
[MAE20191]: Mäurer, N., Gräupl, T., and C. Schmitt, "Evaluation of the LDACS Cybersecurity Implementation", IEEE 38th Digital Avionics Systems Conference (DACS), pp. 1-10, San Diego, CA, USA , 2019.
[MAE20192]: Mäurer, N. and C. Schmitt, "Towards Successful Realization of the LDACS Cybersecurity Architecture: An Updated Datalink Security Threat- and Risk Analysis", IEEE Integrated Communications, Navigation and Surveillance Conference (ICNS), pp. 1-13, Herndon, VA, USA , 2019.
[MAE20182]: Mäurer, N. and A. Bilzhause, "A Cybersecurity Architecture for the L-band Digital Aeronautical Communications System (LDACS)", IEEE 37th Digital Avionics Systems Conference (DASC), pp. 1-10, London, UK , 2017.
[GRA2011]: Gräupl, T. and M. Ehammer, "L-DACS1 Data Link Layer Evolution of ATN/IPS", 30th IEEE/AIAA Digital Avionics Systems Conference (DASC), pp. 1-28, Seattle, WA, USA , 2011.
[GRA2018]: Gräupl, T., Schneckenburger, N., Jost, T., Schnell, M., Filip, A., Bellido-Manganell, M.A., Mielke, D.M., Mäurer, N., Kumar, R., Osechas, O., and G. Battista, "L-band Digital Aeronautical Communications System (LDACS) flight trials in the national German project MICONAV", Integrated Communications, Navigation, Surveillance Conference (ICNS), pp. 1-7, Herndon, VA, USA , 2018.
[ICAO2022]: International Civil Aviation Organization (ICAO), "L-Band Digital Aeronautical Communication System (LDACS", International Standards and Recommended Practices Annex 10 - Aeronautical Telecommunications, Vol. III - Communication Systems, 2022 , 2022.
[SAJ2014]: Haindl, B., Meser, J., Sajatovic, M., Müller, S., Arthaber, H., Faseth, T., and M. Zaisberger, "LDACS1 Conformance and Compatibility Assessment", IEEE/AIAA 33rd Digital Avionics Systems Conference (DASC), pp. 1-11, Colorado Springs, CO, USA , 2014.
[RIH2018]: Rihacek, C., Haindl, B., Fantappie, P., Pierattelli, S., Gräupl, T., Schnell, M., and N. Fistas, "L-band Digital Aeronautical Communications System (LDACS) Activities in SESAR2020", Integrated Communications Navigation and Surveillance Conference (ICNS), pp. 1-8, Herndon, VA, USA , 2018.
[BEL2019]: Bellido-Manganell, M. A. and M. Schnell, "Towards Modern Air-to-Air Communications: the LDACS A2A Mode", IEEE/AIAA 38th Digital Avionics Systems Conference (DASC), pp. 1-10, San Diego, CA, USA , 2019.
[CRO2016]: Crowe, B., "Proposed AeroMACS PKI Specification is a Model for Global and National Aeronautical PKI Deployments", WiMAX Forum at 16th Integrated Communications, Navigation and Surveillance Conference (ICNS), pp. 1-19, New York, NY, USA , 2016.
[MAE2020]: Mäurer, N., Gräupl, T., and C. Schmitt, "Comparing Different Diffie-Hellman Key Exchange Flavors for LDACS", IEEE/AIAA 39th Digital Avionics Systems Conference (DASC), pp. 1-10, San Antonio, TX, USA , 2020.
[STR2016]: Strohmeier, M., Schäfer, M., Pinheiro, R., Lenders, V., and I. Martinovic, "On Perception and Reality in Wireless Air Traffic Communication Security", IEEE Transactions on Intelligent Transportation Systems, 18(6), pp. 1338-1357, New York, NY, USA , 2016.
[BIL2017]: Bilzhause, A., Belgacem, B., Mostafa, M., and T. Gräupl, "Datalink Security in the L-band Digital Aeronautical Communications System (LDACS) for Air Traffic Management", IEEE Aerospace and Electronic Systems Magazine, 32(11), pp. 22-33, New York, NY, USA , 2017.
[MAE20181]: Mäurer, N. and A. Bilzhause, "Paving the Way for an IT Security Architecture for LDACS: A Datalink Security Threat and Risk Analysis", IEEE Integrated Communications, Navigation, Surveillance Conference (ICNS), pp. 1-11, New York, NY, USA , 2018.
[FAA2020]: FAA, "Federal Aviation Administration. ADS-B Privacy.", August 2020, <https://www.faa.gov/nextgen/equipadsb/privacy/>.
[GNU2021]: GNU Radio project, "GNU radio", October 2021, <http://gnuradio.org>.
[SIT2020]: SITA, "Societe Internationale de Telecommunications Aeronautiques", August 2020, <https://www.sita.aero/>.
[ARI2020]: ARINC, "Aeronautical Radio Incorporated", August 2020, <https://www.aviation-ia.com/>.
[DO350A]: RTCA SC-214, "Safety and Performance Standard for Baseline 2 ATS Data Communications (Baseline 2 SPR Standard)", May 2016, <https://standards.globalspec.com/std/10003192/rtca-do-350-volume-1-2>.
[ICAO2019]: International Civil Aviation Organization (ICAO), "Manual on VHF Digital Link (VDL) Mode 2, Doc 9776", January 2019, <https://store.icao.int/en/manual-on-vhf-digital-link-vdl-mode-2-doc-9776>.
[KAMA2010]: Kamali, B., "An Overview of VHF Civil Radio Network and the Resolution of Spectrum Depletion", Integrated Communications, Navigation, and Surveillance Conference, pp. F4-1-F4-8 , May 2010.
[KAMA2018]: Kamali, B., "AeroMACS: An IEEE 802.16 Standard-based Technology for the Next Generation of Air Transportation Systems", John Wiley and Sons, DOI: 10.1002/9781119281139 , September 2018.
[NIST2013]: Barker, E., "Digital Signature Standard (DSS)", National Institute of Standards and Technology (NIST), FIPS.186-4, DOI: 10.6028/NIST.FIPS.186-4 , 2013.
[SON2021]: Soni, D., Basu, K., Nabeel, M., Aaraj, N., Manzano, M., and R. Karri, "FALCON", Hardware Architectures for Post-Quantum Digital Signature Schemes, pp. 31-41 , November 2021.
[AVA2021]: Avanzi, R., Bos, J., Ducas, L., Kiltz, E., Lepoint, T., Lyubashevsky, C., Schanck, J.M., Schwabe, P., Seiler, G., and D. Stehle, "CRYSTALS-KYBER - Algorithm Specification and Supporting Documentation (version 3.02)", August 2021, <https://pq-crystals.org/kyber/data/kyber-specification-round3-20210804.pdf>.
[ROY2020]: Roy, S.S.. and A. Basso, "High-Speed Instruction-Set Coprocessor For Lattice-Based Key Encapsulation Mechanism: Saber In Hardware", IACR Transactions on Cryptographic Hardware and Embedded Systems, 443-466. , August 2020.
[RAW-TECHNOS]: Thubert, P., Cavalcanti, D., Vilajosana, X., Schmitt, C., and J. Farkas, "Reliable and Available Wireless Technologies", Work in Progress, Internet-Draft, draft-ietf-raw-technologies-06, 30 November 2022, <https://www.ietf.org/archive/id/draft-ietf-raw-technologies-06.txt>.
[RAW-USE-CASES]: Bernardos, C. J., Papadopoulos, G. Z., Thubert, P., and F. Theoleyre, "RAW Use-Cases", Work in Progress, Internet-Draft, draft-ietf-raw-use-cases-08, 22 October 2022, <https://www.ietf.org/archive/id/draft-ietf-raw-use-cases-08.txt>.
[I-D.haindl-lisp-gb-atn]: Haindl, B., Lindner, M., Moreno, V., Portoles-Comeras, M., Maino, F., and B. Venkatachalapathy, "Ground-Based LISP for the Aeronautical Telecommunications Network", Work in Progress, Internet-Draft, draft-haindl-lisp-gb-atn-08, 23 September 2022, <https://www.ietf.org/archive/id/draft-haindl-lisp-gb-atn-08.txt>.
[I-D.ietf-rtgwg-atn-bgp]: Templin, F., Saccone, G., Dawra, G., Lindem, A., and V. Moreno, "A Simple BGP-based Mobile Routing System for the Aeronautical Telecommunications Network", Work in Progress, Internet-Draft, draft-ietf-rtgwg-atn-bgp-19, 6 November 2022, <https://www.ietf.org/archive/id/draft-ietf-rtgwg-atn-bgp-19.txt>.
[I-D.ietf-lisp-rfc6830bis]: Farinacci, D., Fuller, V., Meyer, D., Lewis, D., and A. Cabellos-Aparicio, "The Locator/ID Separation Protocol (LISP)", Work in Progress, Internet-Draft, draft-ietf-lisp-rfc6830bis-38, 7 May 2022, <https://www.ietf.org/archive/id/draft-ietf-lisp-rfc6830bis-38.txt>.
[I-D.ietf-lisp-rfc6833bis]: Farinacci, D., Maino, F., Fuller, V., and A. Cabellos-Aparicio, "Locator/ID Separation Protocol (LISP) Control Plane", Work in Progress, Internet-Draft, draft-ietf-lisp-rfc6833bis-31, 2 May 2022, <https://www.ietf.org/archive/id/draft-ietf-lisp-rfc6833bis-31.txt>.
[ICAO2018]: International Civil Aviation Organization (ICAO), "Handbook on Radio Frequency Spectrum Requirements for Civil Aviation, Doc 9718, Volume 1, ICAO Spectrum Strategy, Policy Statements and Related Information", July 2018, <https://www.icao.int/safety/FSMP/Documents/Doc9718/Doc9718_Vol_I_2nd_ed_(2018)corr1.pdf>.
[ARI2019]: ARINC, "AOC Air-Ground Data And Message Exchange Format, ARINC 633", January 2019, <https://standards.globalspec.com/std/13152055/ARINC%20633>.
[VIR2021]: Virdia, A., Stea, G., and G. Dini, "SAPIENT: Enabling Real-Time Monitoring and Control in the Future Communication Infrastructure of Air Traffic Management", IEEE Transactions on Intelligent Transportation Systems, 22(8):4864-4875 , August 2021.
[SHU2013]: Shutin, D., Schneckenburger, N., Walter, M., and M. Schnell, "LDACS1 Ranging Performance - An Analysis Of Flight Measurement Results", IEEE 32nd Digital Avionics Systems Conference (DASC), pp. 1-10, East Syracuse, NY, USA , October 2013.
[BEL2021]: Bellido-Manganell, M.A., Gräupl, T., Heirich, O., Mäurer, N., Filip-Dhaubhadel, A., Mielke, D.M., Schalk, L.M., Becker, D., Schneckenburger, N., and M. Schnell, "LDACS Flight Trials: Demonstration and Performance Analysis of the Future Aeronautical Communications System", IEEE Transactions on Aerospace and Electronic Systems, pp. 1-19 , September 2021.
[MAE2021]: Mäurer, N., Gräupl, T., Gentsch, C., Guggemos, T., Tiepelt, M., Schmitt, C., and G. Dreo Rodosek, "A Secure Cell-Attachment Procedure for LDACS", 1st Workshop on Secure and Reliable Communication and Navigation in the Aerospace Domain (SRCNAS), pp. 1-10, Vienna, Austria , September 2021.
[MAE20211]: Mäurer, N., Gräupl, T., Bellido-Manganell, M.A., Mielke, D.M., Filip-Dhaubhadel, A., Heirich, O., Gerberth, D., Flux, M., Schalk, L.M., Becker, D., Schneckenburger, N., and M. Schnell, "Flight Trial Demonstration of Secure GBAS via the L-band Digital Aeronautical Communications System (LDACS)", IEEE Aerospace and Electronic Systems Magazine, 36(4), pp. 8-17 , April 2021.
[BOE2019]: Boegl, T., Rautenberg, M., Haindl, R., Rihacek, C., Meser, J., Fantappie, P., Pringvanich, N., Micallef, J., Klauspeter, H., MacBride, J., Sacre, P., v.d. Eiden, B., Gräupl, T., and M. Schnell, "LDACS White Paper - A Roll-out Scenario", International Civil Aviation Organization, Communications Panel - Data Communications Infrastructure Working Group - Third Meeting, pp. 1-8, Montreal, Canada , October 2019.

	RCP 130	RCP 130
Parameter	ET	TT95%
Transaction Time (sec)	130	67
Continuity	0.999	0.95
Availability	0.989	0.989
Integrity	1E-5 per FH	1E-5 per FH

	RCP 240	RCP 240	RCP 400	RCP 400
Parameter	ET	TT95%	ET	TT95%
Transaction Time (sec)	240	210	400	350
Continuity	0.999	0.95	0.999	0.95
Availability	0.989	0.989	0.989	0.989
Integrity	1E-5 per FH	1E-5 per FH	1E-5 per FH	1E-5 per FH

	RSP 160	RSP 160	RSP 180	RSP 180	RSP 400	RSP 400
Parameter	OT	DT95%	OT	DT95%	OT	DT95%
Transaction Time (sec)	160	90	180	90	400	300
Continuity	0.999	0.95	0.999	0.95	0.999	0.95
Availability	0.989	0.989	0.989	0.989	0.989	0.989
Integrity	1E-5 per FH	1E-5 per FH	1E-5 per FH	1E-5 per FH	1E-5 per FH	1E-5 per FH