Comparison of inverse optimal and tuning functions designs for adaptive missile control

Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference 2007

Volumn 3, Issue , 2007, Pages 3229-3248

  Sonneveldt, L ^a,b   Van Oort, E R ^a,b   Chu, Q P ^a   Mulder, J A ^a  

^a DELFT UNIVERSITY OF TECHNOLOGY   (Netherlands)

^b Aerospace Software and Technology Institute   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; AERODYNAMICS; COMPUTER SIMULATION; CONTROL EQUIPMENT; LYAPUNOV FUNCTIONS; UNCERTAINTY ANALYSIS;

ADAPTIVE BACKSTEPPING; NONLINEAR MISSILE MODELS; REFERENCE SIGNALS; TUNING FUNCTIONS;

MISSILES;

EID: 37249012816     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-6675     Document Type: Conference Paper

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