Title: VDL Mode 4 Airborne Architecture Study VM4AAS
1VDL Mode 4Airborne Architecture Study(VM4AAS)
- Study Overview and Conclusions
E. F. Charles LaBerge, PhD Honeywell AES
Laboratory Communications Surveillance Center
of Excellence
Nikos Fistas EATMP / EUROCONTROL Communications
Surveillance Management Business Division
2Presentation Overview
- PART I General information (ECTL)
- Scope, Objectives, Plan, Structure
- PART II Study Summary (Honeywell)
- Overview of work achieved (Work Packages 1 to 4)
- Conclusions
- Recommendations
- Next Steps
3PART IGENERAL INFORMATION
4VM4AAS scope
- Investigate airborne integration issues for VDL
Mode 4, considering - COM / SUR / COM and SUR applications
- Large / Small / Light a/c
- Forward-fit / Retrofit (digital and analogue)
a/c
5VM4AAS Objectives (contd)
- To
- provide answers to questions
- identify potential problems
- make recommendations
- contribute to decision making
- provide input/guidance to manufacturers
- considering current status and future trends
6Study Background Information
- Performed by Honeywell
- Started in June 2002
- Finished October 2003
- Informal external review group (open to
interested volunteers )
7VM4AAS Deliverables
8Deliverable Review Process
9PART IISTUDY SUMMARY
10VM4AAS Work Structure
- Preparatory work
- WP1 - D1 Assumptions and Baselines
- WP2 - D2 Identifications of Requirements
- Investigations
- WP3 - D3.2 RF Interference Analysis
- WP3 - D3.1 Avionics Architectures
- WP4 - D4 Implementation and Transition
11Work Package 1 Assumptions and Baselines
- Preliminary work to form the foundation for WP3
- Establish assumptions
- Establish baselines
12WP1 Assumptions
- VDL Mode 4 is acceptable to support applications
- CDL only
- SDL only
- combined CDL and SDL
- 15 other assumptions in 3 broad groups
- Group 1
- SSR
- Mode-S-based ACAS
- Group 2
- Simultaneous VHF Communications
- Group 3
- 8.33 kHz VHF Voice will be required throughout
the study period
13WP1 Aircraft Classes
- Large take-off mass gt15,000 kg
- (Citation X, G-IV, ERJ, Airbus, Boeing)
- Small 5700 kg lt take-off mass lt 15,000 kg
- (King Air 350, most Citation)
- Light take-off mass lt 5700 kg
- (Cessna 172, King Air C90B)
14WP1 Equipment Baselines (1)
- Communication
- VHF Voice (DSB-AM) x 2
- ACARS or Mode 2
- Simultaneous operation of voice and data link
- Navigation
- GNSS
- ILS (Localizer and Glideslope)
- VOR
15WP1 Equipment Baselines (2)
- Surveillance
- Mode S Transponder 1
- Mode S Transponder 2 or Mode C
- ACAS Mode S Interrogator (Large Small)
- CDTI
16Work Package 2Identification of Requirements
- Identify general functional requirements
- Identify internal interfaces
- Identify external interfaces
17WP2 Internal Interfaces
- Interconnections
- VDLM4 to and from other avionics
- Data Flow Diagrams
- Data Dictionary
- Precision Time Interface (PTI)
- CONCLUSION
- Only PTI and baseband interface issues are unique
to VDL Mode 4 compared to any other CDL/SDL
modem technology
18WP2 Context-Level DFD
- An example Level 1 - external interactions
19WP2 External Interface Issues
- RF Interference to/from other avionics
- Focus on same-aircraft or co-site problems
- Detailed study in WP3.2
- Derived work on integrity, availability, and
continuity of service - Traffic Loading estimates for 2015 based on
MACONDO
20Work Package 3.2Interference Analysis (1)
- RF Interference Issues
- VHF Communications
- Sources DSB-AM, VDL Mode 2, VDL Mode 4
- Victims DSB-AM, VDL Mode 4, Localizer, VOR,
VDB, Glideslope - Large, Small, Light Aircraft
21Work Package 3.2Interference Analysis (2)
- Same-side, Opposite-side antennas
- Link-budget analysis using published standards or
carefully documented assumptions - 3 issues Desensitization, Off-Channel Emissions,
RF (front end) Saturation
22WP3.2 VHF COM I/f Problem
23WP3.2 Key Assumptions
- MOPS -87 dBm reference signal level
- Emissions levels
- DO-186A (Voice), DO-281/ED-92 (Mode 2), ED108
(Mode 4) - Assumed noise floors
- Using ARINC 716 isolations
- MOPS adjacent channel rejection
- ACR is a desensitization spec
- Figure of merit Es/N0 or S/P
24WP3.2 3 VHF-on-VHF i/f scenarios
- Voice on digital
- RF Saturation
- IF Desensitization
- Off-channel emissions (residual phase noise)
- Digital on voice
- RF Saturation
- Squelch break
- Audio S/P concerns
- Digital on digital
- RF Saturation
- Desensitization IF
- Off-Channel emissions (residual phase noise)
- Potential duty-factor mitigation
25WP3.2 Voice on digital i/f
- Mechanism
- Primarily phase noise and RF saturation
- IF desensitization is lesser effect
- Challenges
- 100 voice duty factor
- Voice transmitter 46 dBm (40 W)
- Mitigations
- Better in-band filtering for digital receiver
(IF) - Better-than-MOPS phase noise of voice
transmitter - Increased isolation
- Channel separation
- Robust application protocols
- Clear continuity definitions
- Reduced use of AM voice as data use increases
26WP3.2 Digital on voice i/f
- Mechanism
- Primarily phase noise and RF saturation
- IF desensitization is lesser effect
- Challenges
- 100 voice duty factor
- Better than MOPS sensitivity of most AT receivers
- Mitigations
- Better than MOPS emissions for digital
transmitter - Increased isolation
- Channel separation
- Constrain protocols to short pulse widths
- Consider cooperative suppression during
transmissions
27WP3.2 Digital on digital i/f
- Mechanism
- Primarily phase noise and RF saturation
- IF desensitization is lesser effect
- Challenges
- Multiplicity of antennas/limited isolation
- Low-noise figure designs with FM protection
- Mitigations
- Better emissions for digital transmitter
- Better-than-MOPS adjacent channel rejection
- Increased isolation
- Channel separation
- Robust applications and protocols
- Clear continuity definitions
28WP3.2 Off-channel Desensitization
29WP3.2 RF Saturation
- New result (not in original WP3.2)
- Supported by Boeing/Honeywell testing (Sept 2003
- data not yet released) - May be the limiting factor!
30Work Package 3.1Architecture Descriptions
- 11 different forward fit architectures
- 1 radio retrofit architecture
- Recommendations
- Multi-function VHF radio
- 8.33 kHz, 25 kHz, VDLm2, VDLm4
- Independent transmit and receive capabilities
- Baseband control and flexibility
31WP3.1 requirements and constraints
- Integrity
- RMER 10-6 to 10-8
- Continuity
- Loss of Continuity 1 x 10-5 to 5 x 10-4
- Availability
- Communication system MTBF 1000 days
- Surveillance system MTBF 1000 day
32WP3.1 Architecture Candidate 5
- ARINC 750 form factor New VHF Digital Radio
(NVDR) - 4R1T, half duplex transceivers (not available
today) - High-speed baseband information sharing
- Independently reconfigurable R/T capabilities
33WP3.1 Architecture Candidate 9
- Remote mount high-end B/RA New VHF Digital Radio
(NVDR) - 4R1T, half duplex transceivers (not available
today) - High-speed baseband information sharing
- Independently reconfigurable R/T capabilities
34WP3.1 Architecture Candidate 10
- Retains existing analog voice radio for GA
aircraft - Small form factor (panel mount?) NVDR
- 4R1T, half duplex transceivers (not available
today) - Independently reconfigurable R/T capabilities
- Somewhat limited under certain failure conditions
35WP3.1 Architecture Candidate 11
- Retains existing analog voice radio for GA
aircraft - Small form factor (panel mount?) NVDR
- 4R1T, half duplex transceivers (not available
today) - Independently reconfigurable R/T capabilities
- Somewhat limited under certain failure conditions
36WP3.1 Other Products
- Allocation table showing how each transmitter and
receiver is used - Availability/continuity analysis tables
- Analytical Appendices
37Work Package 4Implementation and Transition
- Relative normalized costs of installation in a
variety of configurations - Typical and Best-Case schedules
38WP4 Summary of Relative Costs
39WP4 Serial Task Schedule
40WP4 Aggressive Schedule
41Work Package 5 Final Report Summary
- Summarize WPs 1, 2, 3.2, 3.1, and 4
- Review external comments
- Conclusions
- Recommendations
- Open Items and Future Work
42WP5 Review of External Comments
- Comments critical of WP 3.2
- VHF Voice assumptions were too severe
- Worst-case and not statistical analysis
- Not supported by field data and/or trial
experience - Comments about cost analysis with lack of benefit
analysis - Comments about intermodulation
- Comments about saturation
43WP5 Study Conclusions (1)
- Interference Problem
- VHF-on-VHF interference will exist
- VHF-on-VHF interference will prevent simultaneous
voice and data usage (valid for any VDL Mode) - Voice-on-VDL interference is more critical
- Only half-duplex is achievable
- Uplink data applications must be made
sufficiently robust to sustain transfer delay due
to downlink voice - Technical mitigations are insufficient
44WP5 Study Conclusions (2)
- Aircraft Integration Problem
- Recommended architectures are based on
multi-function half-duplex VHF transceiver with 1
TX and 4 RXs - Recommended architectures require interconnected
transceivers - VDL Mode 4 specific integration issues limited to
PTI and baseband connections
45WP5 Study Conclusions (3)
- General
- VDL Mode 4 installation plans should be
coordinated with ADS-B and/or advanced data link
upgrades - Simultaneous operation of multiple VDLs and voice
should be avoided - Relative installation costs Retrofit analog gt
Retrofit Digital gt Forward fit
46WP5 Study Recommendations (1)
- Investigate operational impact of VDL Mode 4
interference to voice and vice versa to determine
if and which applications can be supported - Complete feasibility analysis (safety, ..) of
recommended architectures and facilitate as
appropriate the development of multi-function
4R1T transceiver with - 8.33/25 kHz analog voice, VDL Mode 2, VDL Mode 4
- common baseband coordination
- quasi-independent R/T functions
- Use VMAAS results as input to other efforts to
complete VDL Mode 4 specific cost/benefit
analysis (CBA) to support link decision - Coordinate any aircraft upgrades with ADS-B and
advanced CDL application upgrades
47WP5 Open Items/Future Work (1)
- Assess operational impact of voice-on-data
interference - Adopt GFSK BER analysis as part of a standard for
reference - Adopt VDL Mode 4 link budget to level of detail
comparable with other VDL data links
48WP5 Open Items/Future Work (2)
- Perform or refine system-level cost benefit
analysis based on relative costs provided by WP4 - Perform, publish, and publicize additional
measurements of VHF-on-VHF interference effects
49VM4AAS
- Remarks Questions
- More info and available draft deliverables
- www.eurocontrol.int/vdl4/architecture.html
- Comments and input welcome
- nikolaos.fistas_at_eurocontrol.int
- christophe.hamel_at_honeywell.com
- chuck.laberge_at_honeywell.com