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Avionics, systems design and simulation

Published online by Cambridge University Press:  04 July 2016

D. J. Allerton
D. J. Allerton*
Affiliation:
College of Aeronautics , Cranfield University, UK
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Abstract

The paper reviews the developments in avionics over the last seventy years, focusing on the impact of computer technology during the last ten years. The development of aircraft navigation systems is described, including present day satellite navigation and terrain reference navigation. The techniques used in aircraft displays are outlined including CRTs and LCDs and covering head up displays, helmet mounted displays and synthetic displays. The systems architecture which forms the basis of modem avionics is described, covering the major aircraft databuses in use including recent developments in integrated modular avionics. Developments in real-time software, which has become a major cost in many programmes, are covered, leading to the techniques used to ensure aircraft reliability, particularly fault tolerant architectures and also safety systems for health monitoring and recent research in ‘pilot associates'. The paper also summarises developments in flight control systems for both civil and military aircraft. The paper concludes with a brief review of future developments in avionics, speculating on the role of pilot in future aircraft.

Type
Research Article
Information
The Aeronautical Journal , Volume 100 , Issue 1000 , December 1996 , pp. 438 - 448
Copyright
Copyright © Royal Aeronautical Society 1996 

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References

1. Grocott, D.F.H. Options for the future, Nav 91, Royal Institute of Navigation, London, November 1991.Google Scholar
2. Wilkes, M.V. The CMOS end-point and related topics in computing, IEE Comp CntlJ. April 1996, 7, (2), pp 101–106.Google Scholar
3. Helfrick, A.D. Modem Aviation Electronics, Prentice Hall, 1996.Google Scholar
4. Gething, P.J.D. Radio Direction Finding and the Resolution of Multi- component Wave Fields, Peter Pereginus, 1978.Google Scholar
5. Forsell, B. Radionavigation Systems, Prentice Hall, 1991.Google Scholar
6. Kelly, R.J. System consideration for the new DME/P international standard, IEEE Trans Aerospace and Electronics-20, 1984, (1).Google Scholar
7. Redlien, H.W. and Kelly, R.J. Microwave landing system: the new international standard, Advances in Electronics and Electron Physics, 57, Academic Press, 1984.Google Scholar
8. Van Etten, E.R. Navigation systems: fundamentals of low and very low frequency hyperbolic techniques, Elec Comms, 1970, 45, (2), pp 192–212.Google Scholar
9. Last, J.D. and Linsdall, D.K. Automatic microprocessor-based receivers for the Decca navigator system, The Radio and Electronic Engineer, 1984, 54, (7/8).Google Scholar
10. Pierce, J.A. Omega, IEEE Trans Aerospace and Electronic Systems, AES-1, December 1965, (6).Google Scholar
11. Poppe, M.C. The Loran-C receiver — a functional description. Navigation, 1982, 29,(1).Google Scholar
12. De Lorme, J.F. and Tuppen, A.R. Low-cost airborne Loran-C navigator, Elec Comms, 1975, 50, (4).Google Scholar
13. Gupta, R.R. and Morris, P.B. Omega navigation signal characteristics, Navigation, 1986, 33, (3).Google Scholar
14. Farrell, J.L. Integrated Aircraft Navigation, Academic Press, 1976.Google Scholar
15. Savage, P. Strap-down Sensors, AGARD Lecture series No. 95, Strap-down Inertial Systems, 1978, pp 21-46.Google Scholar
16. Roland, J.J. and Agrawal, G.P. Optical gyroscopes. Optics and Laser Technology, October 1981, pp 239–244.Google Scholar
17. Cox, D.B. Integration of GPS with inertial navigation systems, Navigation, 1978, 25, (2), pp 236–245.Google Scholar
18. Siouris, G.M. Aerospace Avionics Systems, Academic Press, 1993.Google Scholar
19. Harris, R.L. Introduction to spread spectrum methods, AGARD Lecture Series, 1973,(58).Google Scholar
20. Klobuchar, J.A. Ionospheric time-delay algorithm for single frequency GPS users, IEEE Trans Aerosp Elect, 1987, 23, (3).Google Scholar
21. Blackwell, E.G. Overview of Differential GPS methods, Navigation, 1986, III, pp 89–100.Google Scholar
22. Daly, P. and Lennon, G.E. Potential for an integrated GPS/Glonass civil navigation system, Nav 89, Royal Institute of Navigation, London, October 1989.Google Scholar
23. Hewitt, C., Henley, A.J. and Boyes, J.D. A ground and obstacle collision avoidance technique (GOCAT), IEEE National Aerospace and Electronics Conf. (NAECON), 1991 pp 604–610.Google Scholar
24. Allerton, D.J. and Gia, M.C. Oct-tree terrain modelling methods for terrain reference navigation systems, Aeronaut J, May 1996, pp 157–163.Google Scholar
25. Zelenka, R.E. Integration of radar altimeter, precision navigation and digital terrain data for low-altitude flight, AIAA-92-4420-CP, 1992, pp 605–615.Google Scholar
26. OrlandoV A, , The Mode-S beacon radar system, Lincoln Laboratory, 1989, 2, (3).Google Scholar
27. Ford, R.L. The protected volume of airspace generated by an airborne collision avoidance system, J Nav, May 1986, 39, (2), pp 139–158.Google Scholar
28. Smith, J.H. Colour multi-function displays for aircraft, Nav 87, Royal Institute of Navigation, 1987.Google Scholar
29. Koniche, M.L. 747-400 Flight Displays Development, AIAA Aircraft Design, Systems and Operations Conf., AIAA 88-4439, Atlanta, September 1988.Google Scholar
30. Lucas, E. Flat panel displays, Avionics, June 1992, pp 60–66.Google Scholar
31. Bartlett, C.T. A practical application of computer generated hologra phy to head up display design, Displays, 1996, 15, (2).Google Scholar
32. Adam, E.C. Head up displays versus helmet mounted displays — the issues, SPIE, April 1996, 2219, pp 13–21.Google Scholar
33. Burgess, M.A. and Hayes, R.D. Synthetic vision — a view in the fog, IEEE 1 1th Digital Avionics System Conference, Seattle, October 1992.Google Scholar
34. Bracknell, D.R. Introduction to the MIL-STD-1553B serial multiplex data bus, Microprocessors Microsystems J, January 1988, 12,(1).Google Scholar
35. Gillen, A. and Joung, S. A primer on Stanag-3910, Avionics, June 1992, pp 38–44.Google Scholar
36. Moore, J.F. and Shorland, M. ARINC 629 status and terminal design, Proc. ARINC 629 Databus Conference, Royal Aeronautical Society, pp 2.1–2.16, London, September 1991.Google Scholar
37. Morgan, M.J. Integrated modular avionics for next generation com mercial airplanes, IEEE Aerospace and Electronics Systems, August 1991, 6, (8), pp 9–12.Google Scholar
38.DO-178B/ED-12B, RTCA-EUROCAE, Software Considerations in Airborne Systems and Equipment Certification, December 1992.Google Scholar
39.ARINC Report 613, Guidance for Using the ADA Programming Language in Avionics Systems, 1987.Google Scholar
40.ARINC Report 604, Guidance for Design and Use of Built-in Test Equipment.Google Scholar
41. The Future Flight Deck, Discussion Paper, Flight Operations Group, Royal Aeronautical Society, 1994.Google Scholar
42. Lambert, R.E., Keller, K.J. and Meyer, S.A. Pilot's Associate, AIAA Guidance and Control Conference, pp 1–9, New Orleans, August 1991.Google Scholar
43. Gibson, J.C. Piloted handling qualities design criteria for high order flight control systems, AGARD CP-333, 1982.Google Scholar
44. Wiener, E.L. Human factors of advanced technology (“glass cockpit“) transport aircraft, NASA CR-177528, June 1989.Google Scholar
45. Allen, L. Evolution of flight simulation, AIAA Flight Simulation and Technologies Conference, Vol. AIAA-93-3545, Monterey, 1993.Google Scholar