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http://dx.doi.org/10.5302/J.ICROS.2003.9.7.547

Adaptive Control Based on a Parametric Affine Model for Tail-Controlled Missiles  

최진영 (서울대학교 전기공학부)
좌동경 (서울대학교 전기공학부)
송찬호 (국방과학연구소)
Publication Information
Journal of Institute of Control, Robotics and Systems / v.9, no.7, 2003 , pp. 547-555 More about this Journal
Abstract
This paper presents an adaptive control against uncertainties in tail-controlled STT (Skid-to-Turn) missiles. 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.
Keywords
adaptive control; STT missiles; analytic uncertainty model; parametric affine missile model;
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