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http://dx.doi.org/10.5302/J.ICROS.2004.10.7.658

Mixed Control of Agile Missile with Aerodynamic Fin and Thrust Vectoring Control  

이호철 (부산대학교 기계공학부)
최용석 (삼성전)
송택렬 (한양대학교 전자컴퓨터공학)
송찬호 (국방과학연구)
최재원 (부산대학교 기계공학부 및 기계기술연구소)
Publication Information
Journal of Institute of Control, Robotics and Systems / v.10, no.7, 2004 , pp. 658-668 More about this Journal
Abstract
This paper is concerned with a control allocation strategy using the dynamic inversion and the pseudo inverse control which generates the nominal control input trajectories. In addition, an autopilot design method is proposed by using time-varying control technique which is time-varying version of the pole placement of linear time-invariant system for an agile missile with aerodynamic fin and thrust vectoring control. The control allocation proposed in this paper is capable of extracting the maximum performance by combining each control effector, aerodynamic fin and thrust vectoring control. The adopted time-varying control technique for the autopilot design enhances the robustness of the tracking performance for a reference command. The main results are validated through the nonlinear simulations with aerodynamic data.
Keywords
dynamic inversion; extended-mean assignment; control allocation; mixed control; linear time-varying system; autopilot; agile missile;
Citations & Related Records
Times Cited By KSCI : 2  (Citation Analysis)
연도 인용수 순위
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