Robust performance study for lateral autopilot of a quasi-linear parameter-varying missile

Proceedings of the American Control Conference

Volumn 1, Issue , 2002, Pages 226-231

  Bruyere L ^a   Tsourdos, A ^a   Zbikowski, R ^a   White, B A ^a  

^a CRANFIELD UNIVERSITY   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; APPROXIMATION THEORY; CLOSED LOOP CONTROL SYSTEMS; LINEARIZATION; MATHEMATICAL MODELS; MISSILES; ROBUSTNESS (CONTROL SYSTEMS); SYSTEM STABILITY; UNCERTAIN SYSTEMS;

QUASI-LINEAR PARAMETER VARYING MISSILE; SIDESLIP VELOCITY AUTOPILOT;

CONTROL SYSTEM SYNTHESIS;

EID: 0036057630     PISSN: 07431619     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (6)

1. Autopilots for tactical missiles: An overview
2. Comparison of 6 robustness tests evaluating missile autopilot robustness to uncertain aerodynamics
3. A study of autopilots for the adaptive control of tactical guided missiles
4. Trajectory control of a nonlinear homing missile
5. Robust design of sideslip velocity autopilot for a quasi-linear parameter-varying missile model