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http://dx.doi.org/10.5302/J.ICROS.2004.10.10.947

Mixed Control of Agile Missile with Aerodynamic fin and Side Thrust Control  

최용석 (삼성전자)
이호철 (부산대학교 기계공학부)
송택렬 (한양대학교 전자컴퓨터공학부)
송찬호 (국방과학연구소)
Publication Information
Journal of Institute of Control, Robotics and Systems / v.10, no.10, 2004 , pp. 947-955 More about this Journal
Abstract
This paper is concerned with a mixed control with aerodynamic fin and side thrust control applied to an agile missile using a dynamic inversion and a time-varying control technique. The nonlinear dynamic inversion method with the weighting function allocates the desired control inputs(aerodynamic fin and side thrust control) to achieve a reference command, and the time-varying control technique plays the role to guarantee the robustness for the uncertainties. The proposed schemes are validated by nonlinear simulations with aerodynamic data.
Keywords
dynamic inversion; extended-mean assignment; linear time-varying system; autopilot; mixed control;
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