Robustness of a nonlinear missile autopilot designed using dynamic inversion

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2000, Pages

  McFarland, Michael B ^a   Hoque, Shaheen M ^a  

^a RAYTHEON COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIR NAVIGATION; AIR TO AIR MISSILES; FLIGHT ENVELOPES; INTELLIGENT SYSTEMS; MONTE CARLO METHODS; ROBUSTNESS (CONTROL SYSTEMS); SENSITIVITY ANALYSIS;

AERODYNAMIC PARAMETERS; DESIGN PARAMETERS; GAIN AND PHASE MARGIN; NONLINEAR MISSILE AUTOPILOT; OPTIMAL PERFORMANCE; OUTPUT REDEFINITION; ROBUSTNESS ANALYSIS; SENSITIVITY TO VARIATIONS;

ROBUST CONTROL;

EID: 85086613414     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-3970     Document Type: Conference Paper

References (8)

1. Snell, S.A., Enns, D. F., and Garrard, W.L., "Nonlinear Inversion Flight Control for a Supermaneuverable Aircraft," AIAA Journal of Guidance, Control and Dynamics, Vol. 15, No. 4, pp. 570-577, 1992.
2. Ryu, J. H., Park, C. S., and Tahk, M.J., "Plant Inversion Control of Tail-Controlled Missiles," Proceedings of the AIAA Guidance, Navigation, and Control Conference, pp. 1691-1696, 1997.
3. Sharma, M., Calise, A. J., and Corban, J. E., "Application of an Adaptive Autopilot Design to a Family of Guided Munitions," Submitted to the AIAA Guidance, Navigation, and Control Conference, Denver, 2000.
4. Calise, A. J., Sharma M., and Corban, J. E., "An Adaptive Autopilot Design for Guided Munitions," AIAA Journal of Guidance, Dynamics, and Control, to appear.
5. Drinker, J. S., and Wise, K.A., "Stability and Flying Qualities Robustness of a Dynamic Inversion Aircraft Control Law," AIAA Journal of Guidance, Control, and Dynamics, Vol. 19, No. 6, pp. 1270-1277, 1996.
6. Schumacher, C., and Khargonekar, P., "A Comparison of Missile Autopilot Designs Using HInfinity Control With Gain Scheduling and Dynamic Inversion," Proceedings of the American Control Conference, pp. 2759-2763,1997.
7. Durham, W., "Dynamic Inversion and Model- Following Control," AIAA-96-3690, AIAA Guidance, Navigation, and Control Conference, San Diego, 1996.
8. Bar-On, J. R., and Adams, R.J., "Linearization of a Six-Degree-of-Freedom Missile for Autopilot Analysis," AIAA Journal of Guidance, Control, and Dynamics, Vol. 21, No. 1, pp. 184-187, 1998.