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VDL Mode 4 Airborne Architecture Study VM4AAS

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Low-noise figure designs with FM protection. Mitigations ... WP4: Serial Task Schedule. VDL Mode 4 Airborne Integration Meeting 29/10/03. 40. EUROCONTROL ... – PowerPoint PPT presentation

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Title: VDL Mode 4 Airborne Architecture Study VM4AAS


1
VDL 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
2
Presentation 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

3
PART IGENERAL INFORMATION
4
VM4AAS 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

5
VM4AAS 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

6
Study Background Information
  • Performed by Honeywell
  • Started in June 2002
  • Finished October 2003
  • Informal external review group (open to
    interested volunteers )

7
VM4AAS Deliverables
8
Deliverable Review Process
9
PART IISTUDY SUMMARY
10
VM4AAS 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

11
Work Package 1 Assumptions and Baselines
  • Preliminary work to form the foundation for WP3
  • Establish assumptions
  • Establish baselines

12
WP1 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

13
WP1 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)

14
WP1 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

15
WP1 Equipment Baselines (2)
  • Surveillance
  • Mode S Transponder 1
  • Mode S Transponder 2 or Mode C
  • ACAS Mode S Interrogator (Large Small)
  • CDTI

16
Work Package 2Identification of Requirements
  • Identify general functional requirements
  • Identify internal interfaces
  • Identify external interfaces

17
WP2 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

18
WP2 Context-Level DFD
  • An example Level 1 - external interactions

19
WP2 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

20
Work 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

21
Work 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

22
WP3.2 VHF COM I/f Problem
23
WP3.2 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

24
WP3.2 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

25
WP3.2 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

26
WP3.2 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

27
WP3.2 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

28
WP3.2 Off-channel Desensitization
29
WP3.2 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!

30
Work 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

31
WP3.1 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

32
WP3.1 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

33
WP3.1 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

34
WP3.1 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

35
WP3.1 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

36
WP3.1 Other Products
  • Allocation table showing how each transmitter and
    receiver is used
  • Availability/continuity analysis tables
  • Analytical Appendices

37
Work Package 4Implementation and Transition
  • Relative normalized costs of installation in a
    variety of configurations
  • Typical and Best-Case schedules

38
WP4 Summary of Relative Costs
39
WP4 Serial Task Schedule
40
WP4 Aggressive Schedule
41
Work 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

42
WP5 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

43
WP5 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

44
WP5 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

45
WP5 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

46
WP5 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

47
WP5 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

48
WP5 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

49
VM4AAS
  • 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
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