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Control of V/STOL aircraft

Published online by Cambridge University Press:  04 July 2016

J. A. Franklin
J. A. Franklin*
Affiliation:
Ames Research Center, NASA, Moffett Field, California, USA
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Summary

This paper deals with control of V/STOL aircraft in powered-lift flight. A review of representative operational mission tasks is presented for the take-off, transition, hover and landing flight phases. Characteristics inherent in the basic airframe and propulsion system and the behaviour associated with control augmentation systems are considered. Demands for augmented stability and control response to meet certain mission operational requirements are discussed. Experience from ground-based simulation and flight experiments that illustrates the impact of augmented stability and control on aircraft design is related by example.

Type
Research Article
Information
The Aeronautical Journal , Volume 90 , Issue 895 , May 1986 , pp. 157 - 173
Copyright
Copyright © Royal Aeronautical Society 1986 

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References

1. Anderson, S. B. Historical overview of V/STOL aircraft technology. NASA TM 81280, March 1981.Google Scholar
2. Anon. V/STOL handling, I — criteria and discussion. AGARD R-577-70, December 1970.Google Scholar
3. Chalk, C. R., Key, D. L., Kroll, J. Jr., Wasserman, R., and Radford, R. C. Background information and user guide for MIL-F-83300 — Military specification-flying qualities of piloted V/STOL aircraft. Technical Report AFFDL-TR-70-88, November 1971.Google Scholar
4. Fortenbaugh, R. L. Mathematical models for the aircraft operational environment of DD-963 class ships. Vought Corporation Report 2-55800/8R-3500, September 1978.Google Scholar
5. Brown, R. G. and Camaratta, F. S. Navairengcen ship motion computer program. NAEC MISC-903-8. 1978.Google Scholar
6. Garnett, T. S. Jr. Investigation to study the aerodynamic ship wake turbulence generated by an FF 1052 frigate. Boeing-Vertol Report D210-11140-1, December 1976.Google Scholar
7. Hoh, R. H. and Ashkenas, I. L. Effect of reduced visibility on VTOL handling quality and display requirements. AIAA J Guidance Control March-April 1981, 4, 2.Google Scholar
8. Cooper, G. E. and Harper, R. P. Jr. The use of pilot rating in the evaluation of aircraft handling qualities. NASA TN D-5153, April 1969.Google Scholar
9. Lacey, T. R. MIL-F-83300; View from an aircraft designer. Proceedings, Navy/NASA V/STOL Flying Qualities, April 1977.Google Scholar
10. Anderson, S. B. A comparison of the V/STOL handling qualities of the VAK-191B with the requirements of AGARD Report 577 and MIL-F-83300. NASA TP 1494, July 1979.Google Scholar
11. Rolls, L. S. and Drinkwater, F. J. III. A flight determination of the attitude control power and damping requirements for a visual hovering task in the variable stability and control X-14A research vehicle. NASA TN D-1328, May 1962.Google Scholar
12. Corliss, L. D. Greif, R. K. and Gerdes, R. M. An in-flight simulation of VTOL hover control concepts. AIAA Paper 77–610, June 1977.Google Scholar
13. Hoh, R. H. and Ashkenas, I. L. Development of VTOL flying qualities criteria for low speed and hover. NADC-77052-30, December 1979.Google Scholar
14. Holzhauser, C. A., Morello, S. A., Innis, R. C., and Patton, J. M. Jr. A flight evaluation of a VTOL jet transport under visual and simulated instrument conditions. NASA TN D-6754. March 1972.Google Scholar
15. Shaw, A. W., Lindbeck, R. K., Craig, S. J., and Booth, G. The impact of current V/STOL flying quality control require ments on the propulsion system. AIAA Paper 78–924, July 1978.Google Scholar
16. Fozard, J. W. The British Aerospace Harrier case study in aircraft design. AIAA Professional Study Series, July 1978.Google Scholar
17. Innis, R. C., Holzhauser, C. A., and Quigley, H. C. Airworthiness considerations for STOL aircraft. NASA TN D-5594, January 1970.Google Scholar
18. Scott, B. C., Hynes, C. S., Martin, P. W., and Bryder, R. B. Progress toward development of civil airworthiness criteria for powered-lift aircraft. FAA-RD-76-100 and NASA TM X-73, 124, May 1976.Google Scholar
19. Schroers, L. G. Initial XV-15 flight test results compared to design predictions. AIAA paper 80-0235, January 1980.Google Scholar
20. Anon. YAV-8B aerodynamic stability and control and flying qualities report. McDonnell-Douglas Report MDC A4637, Rev. C, January 1980.Google Scholar
21. Clark, J. W. Jr. and Goldstein, K. W. Status of VTOL and V/STOL flying qualities criteria development — where are we and where are we going? AGARD-CP-333, June 1982.Google Scholar
22. Lebacqz, J. V. and Aiken, E. W. A flight investigation of control, display, and guidance requirements for decelerating descending VTOL instrument transitions using the X-22A variable stability aircraft, Volume I: Technical discussion and results. Calspan Report AK-5336-F-1, September 1975.Google Scholar
23. Merrick, V. K. and Gerdes, R. M. Design and piloted simulation of a VTOL flight control system. AIAA J Guidance Control, May-June 1978, 1, 3.Google Scholar
24. Stapleford, R. L., Clement, W. F., Heffley, R. K., Booth, G. C., and Fortenbaugh, R. L. Flight control/flying qualities investigation for lift/cruise fan V/STOL. NADC Report 77143-30, August 1979.Google Scholar
25. Morello, S. A., Person, L. H. Jr., Shanks, R. E., and Culpepper, R. G. A flight evaluation of a vectored-thrust-jet V/STOL airplane during simulated instrument approaches using the Kestrel (XV-6A) airplane. NASA TN D-6791, May 1972.Google Scholar
26. Gerdes, R. M. and Hynes, C. S. Factors affecting handling qualities of a lift-fan aircraft during steep terminal area approaches. NASA TM X-62, 424, April 1975.Google Scholar
27. Anon. Displays for approach and landing of V/STOL aircraft. AGARD Advisory Report 51, November 1972.Google Scholar
28. Radford, R. C. and Andrisani, D. II. An experimental investigation of VTOL flying qualities requirements in ship board landings. AIAA Paper 80–1625, August 1980.Google Scholar
29. Corliss, L. D. and Dugan, D. C. A VTOL translational rate control systems study on a six degree of freedom motion simulator. NASA TM X-62, 194, October 1972.Google Scholar
30. Brigadier, W. L. Analysis of control actuator authority requirements for attitude and translational rate command augmentation systems for the XV-15 Tilt Rotor research aircraft. NASA TM 81243 and AVRADCOM TR-80-A-13, December 1980.Google Scholar
31. Davis, J., Garnett, T., and Gaul, J. Heavy lift helicopter flight control system. Vol III: Automatic flight control system development and feasibility demonstration. USAAMRDL-TR-77-40C, September 1977.Google Scholar
32. Anon. Tactical aircraft guidance system advanced development program flight test phase report, 1. USAAMRDL-TR-73-89A, April 1974.Google Scholar
33. Merrick, V. K. and Gerdes, R. M. VTOL controls for shipboard operations. SAE Paper 831428, October 1983.Google Scholar
34. Farris, G. G., Merrick, V. K., and Gerdes, R. M. Simulation evaluation of flight controls and display concepts for VTOL shipboard operations. AIAA Paper 83–2173, August 1983.Google Scholar
35. Donley, S. T. Evaluation of several control/display concepts for V/STOL shipboard landing. SAE Paper 801205, October 1980.Google Scholar
36. Tinling, B. E. and Cole, G. L. Simulation study of the interaction between the propulsion and flight control systems of a subsonic lift fan VTOL. NASA TM 81239, 1980.Google Scholar
37. Mihaloew, J. R., Roth, S. P., and Creekmore, R. A real time Pegasus propulsion system model for VSTOL piloted simulation evaluation. AIAA Paper 81-2663 and NASA TM 82770, December 1981.Google Scholar
38. Farley, J. F. Modern flight instrument displays as a major military aviation flight safety weakness. AGARD-CP-347, October 1983.Google Scholar