Investigation and preliminary development of a modified pseudo control hedging for missile performance enhancement

Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference

Volumn 8, Issue , 2005, Pages 6132-6145

  Lam, Quang M ^a,b,c   Hindman, Rick ^a,b,c   Shell, William M ^a,b,c   Ridgely, D Brett ^a,b,c  

^a RAYTHEON COMPANY   (United States)

^b GNC Center   (United States)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; ADAPTIVE CONTROL SYSTEMS; LOOP ANTENNAS; MATHEMATICAL MODELS; REAL TIME SYSTEMS;

AUTOPILOT MISSILES; MISSILE PERFORMANCE ENHANCEMENT; PSEUDO CONTROL HEDGING (PCH); RATE SATURATIONS;

MISSILES;

EID: 29744440894     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-6458     Document Type: Conference Paper

References (14)

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3. Lam, Q., and Barkana, I., "Direct Adaptive Control Treatment to Flight Control Nonlinearity Input Saturation Effects," To Appear, AIAA Guidance, Navigation, and Control Conference, Aug. 2005.
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10. McFarland, M. B., & Hoque, S. M., "Robustness of a Nonlinear Missile Autopilot Designed Using Dynamic Inversion," AIAA Guidance, Navigation, and Control Conference, Aug. 2000.
11. Hindman, R., and Shell, W., "Design of a Missile Autopilot Using Adaptive Nonlinear Dynamic Inversion," American Controls Conference, June 2005.
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13. Menon, P. K., and Ohlmeyer, E. J., "Integrated Guidance-Control Systems for Fixed-Aim Warhead Missiles," AIAA Missile Sciences Conference, Nov. 2000.
14. Lam, Q., Drake, D., and Ridgely, D. B., "Integrated Guidance and Control Design Architecture Via Theta-D/Game Theoretic Mixing," Journal of Guidance, Control & Dynamics (to be published).