Missile longitudinal autopilot design using a new suboptimal nonlinear control method

IEE Proceedings: Control Theory and Applications

Volumn 150, Issue 6, 2003, Pages 577-584

  Xin, M ^a   Balakrishnan, S N ^a  

^a MISSOURI UNIVERSITY OF SCIENCE AND TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

APPROXIMATION THEORY; COMPUTER SIMULATION; CONTROL SYSTEM SYNTHESIS; ELECTRONIC GUIDANCE SYSTEMS; OPTIMAL CONTROL SYSTEMS; PERTURBATION TECHNIQUES; RICCATI EQUATIONS;

HAMILTON-JACOBI-BELLMAN EQUATION; MISSILE LONGITUDINAL AUTOPILOT DESIGN; STATE-DEPENDENT RICCATI EQUATIONS;

NONLINEAR CONTROL SYSTEMS;

EID: 0347024353     PISSN: 13502379     EISSN: None     Source Type: Journal    
DOI: 10.1049/ip-cta:20030966     Document Type: Article

References (10)

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6. McLain, T.W., and Beard, R.W.: 'Nonlinear optimal control design of a missile autopilot'. Presented at the AIAA Conference on Guidance, Navigation and Control, Boston, MA, 10-12 August 1998
7. ∞ control via the state-dependent Riccati equation technique'. Presented at the 1st Int. Conf. on Nonlinear Problems in Aviation and Aerospace, Daytona Beach, FL, May 1996
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9. Mracek, C.P., and Cloutier, J.R.: 'Missile Longitudinal Autopilot Design Using the State-Dependent Riccati Equation Method'. Presented at the Conf. on Nonlinear Problems in Aviation and Aerospace, Daytona Beach, FL, May, 1996
10. Xin, M., and Balakrishnan, S.N.: 'A new method for suboptimal control of a class of nonlinear systems'. Presented at the IEEE Conf. on Decision and Control, Las Vegas, Nevada, 10-13 Dec. 2002