Some control strategies for a high-angle-of-attack missile autopilot

Control Engineering Practice

Volumn 8, Issue 8, 2000, Pages 885-892

  Devaud, E ^a,b   Siguerdidjane, H ^a   Font, S ^a  

^a SUPELEC   (France)

^b ONERA   (France)

Author keywords

[No Author keywords available]

Indexed keywords

APPROXIMATION THEORY; COMPUTER SIMULATION; FEEDBACK CONTROL; LINEARIZATION; MISSILES;

APPROXIMATE FEEDBACK LINEARIZATION; MISSILE AUTOPILOT SYSTEMS;

NONLINEAR CONTROL SYSTEMS;

EID: 0034239051     PISSN: 09670661     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0967-0661(00)00013-7     Document Type: Article

References (23)

1. D.J. Bugajski D.F. Enns Nonlinear control law with application to high angle of attack flight AIAA Journal of Guidance, Control and Dynamics 15 3 1992 761 767
2. A.J. Fossard J. Foisneau T. Hun Huynh Optimisation approchée en boucle fermée des systèmes non linéaires par la méthodologie des perturbations singulières A.J. Fossard D. Normand-Cyrot Systèmes non linéaires Vol. III 1993 Masson Paris
3. Fromion, V. (1995). Une approche incrémentale de la robustesse non linéaire; Application au domaine de l'aéronautique . Ph.D. thesis, Université Paris XI Orsay, France.
4. Fromion, V., Scorletti, G., & Ferreres, G. (1997). Nonlinear performance of a PI controlled missile: An explanation, Proceedings of the 36th IEEE control decision conference , San Diego, CA, (pp. 4198–4203).
5. L.C. Fu W.D. Chang J.H. Yang T.S. Kuo Adaptive robust bank-to-turn missile autopilot design using neural networks AIAA Journal of Guidance, Control and Dynamics 20 2 1997 346 354
6. Gazzina, A. (1988). How to control unstable missile airframes: Methodology and limitations. AGARD conference .
7. Z.J. Geng C.L. McCullough Missile control using fuzzy cerebellar model arithmetic computer neural networks AIAA Journal of Guidance, Control and Dynamics 20 3 1997 557 565
8. J.P. Harcaut Nonlinear control of a missile through a geometric approach A. Bensoussan J.L. Lions Lecture notes in control and information sciences Vol. 144 1990 Springer Berlin 27 36
9. Harcaut, J.P. (1991). Commande non linéaire appliquée au pilotage d'un engin . Ph.D. thesis, ENSAE, France.
10. J. Hauser S. Sastry G. Meyer Nonlinear controller design for flight control systems A. Isidori Nonlinear control system design 1990 Pergamon Press Oxford
11. A. Isidori Nonlinear control systems 1995 Springer New York
12. Lee, J.I., Oh, J.H., Ha, I.J., Kim, E.G., & Cho, H.J. (1996). A new approach to autopilot design for highly nonlinear missiles. AIAA guidance navigation and control conference no. 96–3915.
13. Menon, P.K., & Yousefpor, M. (1996). Design of nonlinear autopilots for high angle of attack missiles. AIAA guidance navigation and control conference no. 96–3913.
14. Nesline, F.N., Wells, B.H., & Zarchan, P. (1979). A combined optimal/ classical approach to robust missile autopilot design. AIAA guidance and control conference no. 79-1731.
15. Nesline, F.W., & Nabbefeld, N.C. (1979). Design of digital autopilots for homing missiles. AGARD conference .
16. ∞ controllers A flight control example IEEE Transactions on Control Systems and Technology 1 2 1993 69 78
17. R.T. Reichert Dynamic scheduling of modern-robust-control autopilot design for missiles IEEE Control Systems Magazine 12 5 1992 35 42
18. J. Reiner G.J. Balas W.L. Garrard Flight control design using robust dynamic inversion and time scale separation Automatica 32 11 1996 1493 1504
19. Scorletti, G. (1997). Approche unifiée de l'analyse et de la commande des systèmes par formulation LMI . Ph.D. thesis, Université Paris XI Orsay, France.
20. J.S. Shamma J.R. Cloutier Gain-scheduled missile autopilot design using linear parameter varying transformation AIAA Journal of Guidance, Control and Dynamics 16 2 1993 256 263
21. H. Siguerdidjane M. Pelegrin Towards a rendezvous problem between an aircraft and automated steering vehicles Control Engineering Practice 4 7 1996 951 955
22. H. Siguerdidjane A possible way to avoid the singularities in automated steering vehicles Proceedings of the eighth IFAC symposium on transportation systems 1 1997 397 400
23. Wu, F., Packard, A., & Balas, G. (1995). LPV Control design for pitch axis missile autopilots. Proceedings of the 34th IEEE control decision conference , New Orleans, LA, (pp. 188–191).