Actuator failure compensation schemes for vibration control of a rocket fairing model

IFAC Proceedings Volumes (IFAC-PapersOnline)

Volumn 36, Issue 5, 2003, Pages 173-178

  Wang, Lingfeng ^a   Tang, Xidong ^a   Tao, Gang ^a   Stankovic, John A ^a  

^a University of Virginia   (United States)

Author keywords

Actuators; Adaptive control; Failure compensation; Launch vehicle payload fairing; Luenberger canonical form; Optimal robust control; Stabilization

Indexed keywords

ACTUATORS; CLOSED LOOP SYSTEMS; FAULT DETECTION; LAUNCH VEHICLES; PLANT MANAGEMENT; ROBUST CONTROL; ROCKETS; STABILIZATION; VIBRATION CONTROL;

ADAPTIVE CONTROL; CANONICAL FORM; FAILURE COMPENSATION; LAUNCH VEHICLE PAYLOADS; OPTIMAL ROBUST CONTROL;

VIBRATION ANALYSIS;

EID: 0142145729     PISSN: 14746670     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1016/S1474-6670(17)36489-3     Document Type: Conference Paper

References (5)

1. S. Griffin, S.A. Lane, C. Hansen, and B. Cazzolato Active structural-acoustic control of a rocket fairing using proof-mass actuators Journal of Spacecraft and Rockets 38 2 2001 219 225
2. J. Lam, and Y.-Y. Cao Simultaneous linear-quadratic optimal control design via static output feedback International Journal of Robust and Nonlinear Control 9 1999 551 558
3. D.G. Luenberger Canonical forms for linear multivariable systems IEEE Transactions on Automatic Control 12 1967 290 293
4. G. Tao, S.H. Chen, and S.M. Joshi An adaptive control scheme for systems with unknown actuator failures Automatica 38 6 2002 1027 1034
5. G. Tao, X.D. Tang, and S.M. Joshi Output tracking actuator failure compensation control Proceedings of the 2001 American Control Conference 2001 1821 1826