Nonlinear simulation of a modified F-16 with full-envelope control laws

Control Engineering Practice

Volumn 6, Issue 3, 1998, Pages 309-320

  Reigelsperger, William C ^a   Banda, Siva S ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

control allocation; dynamic inversion; full envelope control; mu synthesis; robust flight control

Indexed keywords

CONTROL ALLOCATION; DYNAMIC INVERSION; FULL-ENVELOPE CONTROL LAWS;

AIRCRAFT; COMPUTER SIMULATION; CONTROL SYSTEM ANALYSIS; FLIGHT DYNAMICS; MANEUVERABILITY; ROBUSTNESS (CONTROL SYSTEMS);

CONTROL SYSTEM SYNTHESIS;

EID: 0032029597     PISSN: 09670661     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0967-0661(98)00024-0     Document Type: Article

References (20)

1. Adams R.J., Buffington J.M., Banda S.S. Design of nonlinear control laws for high-angle-of-attack flight. Journal of Guidance, Control, and Dynamics. 17(4):1994;737-746.
2. Adams, R.J., Buffington, J.M., Banda, S.S., 1994b. Active vortex flow control for VISTA F-16 envelope expansion. Proc. AIAA Guidance, Navigation, and Control Conference, Scottsdale, AZ, August, 1994.
3. Adams, R.J., Buffington, J.M., Sparks, A.G., Banda, S.S., 1994c. Robust Multivariable Flight Control. Springer-Verlag, London, UK, 1994.
4. Andry A.N., Shapiro E.Y., Chung J.C. Eigenstructure assignment for linear systems. IEEE Transactions on Aerospace and Electronic Systems. AES 19(5):1983;711-724.
5. Bugajski D.J., Enns D.F. Nonlinear control law with application to high angle-of-attack flight. Journal of Guidance, Control, and Dynamics. 15(3):1992;761-767.
6. Doyle, J.C., Lenz, K., Packard, A., 1986. Design examples using μ-synthesis: space shuttle lateral axis FCS during reentry. Proc. 25th IEEE Conference on Decision and Control, Inst. of Electrical and Electronics Engineers, Piscataway, NJ, 1986.
7. Durham W.C. Constrained control allocation. three-moment problem Journal of Guidance, Control, and Dynamics. 17(2):1994;330-336.
8. Enns D.F., Bugajski D.J., Hendrick R., Stein G. Dynamic inversion. an evolving methodology for flight control design International Journal of Control. 59(1):1994;71-91.
9. Gal-Or, B., 1990. Vectored Propulsion, Supermaneuverability and Robot Aircraft, Springer-Verlag, New York, NY, 1990.
10. Hammett, K.D., Reigelsperger, W.C., Banda, S.S., 1995. High angle of attack short period flight control design with thrust vectoring. Proc. American Control Conference, Seattle, WA, June 1995.
11. Huang, C., Knowles, G., Reilly, J., Dayawansa, M., Levine, W., 1990. Analysis and simulation of a nonlinear control strategy for high angle-of-attack maneuvers, presented at the 1990 AIAA Guidance, Navigation, and Control Conf., Portland, OR, Aug 1990.
12. Lane S.H., Stengal R.F. Flight control design using non-linear inverse dynamics. Automatica. 24:1988;471-483.
13. MIL-STD-1797A. Military Standard-Flying Qualities of Piloted Vehicles, 1990.
14. Ostroff A.J., Proffitt M.S. Design and evaluation of a stochastic optimal feed-forward and feedback technology (SOFFT) flight control architecture. 1994;NASA Technical Paper 3419, NASA Langley Research Center, Hampton, VA. June, 1994.
15. Ostroff A.J., Proffitt M.S., Hoffler K.D. High-alpha research vehicle (HARV) longitudinal controller. design, analysis, and simulation results:1994;NASA Technical Paper 3446, NASA Langley Research Center, Hampton, VA. July, 1994.
16. Reigelsperger, W.C., Hammett, K.D., Brada, S.S., 1996. Robust control law design for lateral-directional modes of an F-16/MATV using μ-synthesis and dynamic inversion, to appear in the International Journal of Robust and Nonlinear Control, 1996.
17. Safonov M.G., Chiang R.Y. Model reduction for robust control. a Schur relative error method International Journal of Adaptive Control and Signal Processing. 2:1988;259-272.
18. Sparks A.G., Banda S.S. Application of structured singular value synthesis to a fighter aircraft. Journal of Guidance, Control and Dynamics. 16(5):1993;940-947.
19. WL-TR-91-3105, 1991. Robust Control Law Development for Modern Aerospace Vehicles.
20. WL-TR-96-3099, 1996. Multivariable Control Design Guidlelines.