24th Congress of International Council of the Aeronautical Sciences, 29 August-3, September 2004, Yokohama, Japan
Paper ICAS 2004-7.1.3 (St.)

CONTROL ALLOCATION AND AUTOPILOT DESIGN FOR AGILE MISSILE

H. C. Lee, J. W. Choi , Y. S. Choi*
School of Mechanical Engineering, Pusan National University, Korea; *Samsung Electronics Co., Ltd., Korea

Keywords: Time-Varying Control, Control Allocation, Dynamic Inversion, Autopilot

This paper is concerned with the control allocation strategies with the two-time scale dynamic inversion which generate nominal control input trajectories. In addition, an robust flight control design method is proposed by using a time-varying control technique which is a time-varying version of the pole placement of the linear time-invariant system for an agile missile with aerodynamic fin, thrust vectoring control, and side-jet thruster.

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