An adaptive control against uncertainties in tail-controlled STT (skid-to-turn) missiles is presented. First, we derive an analytic uncertainty model from a parametric affine missile model developed by the authors. Based on this analytic model, an adaptive feedback linearizing control law accompanied by a sliding mode control law is proposed. We provide analyses of stability and output tracking performance of the overall adaptive missile system. The performance and validity of the proposed adaptive control scheme are demonstrated by simulation.
Adaptive control based on a parametric affine model for tail-controlled missiles
IEEE Transactions on Aerospace and Electronic Systems ; 42 , 2 ; 659-669
2006-04-01
1205070 byte
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Adaptive Control Based on a Parametric Affine Model for Tail-Controlled Missiles
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