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Guidance & Control System Design based on Optimization  

Moon, Gwan-Young (Agency for Defense Development)
Jun, Byung-Eul (Agency for Defense Development)
Publication Information
Journal of the Institute of Electronics Engineers of Korea SC / v.48, no.5, 2011 , pp. 52-58 More about this Journal
Abstract
The missile control system is comprised of various control systems such as autopilot, guidance law, and homing filter and so on. To design these guidance and control system, the optimization technique is widely applied at each developing stage. However, this kind of optimization requires lots of time and cost and moreover, this approach does not give an overall system optimization result. In this paper, to use the optimization tool for control system design, the optimal problem formulation is done and the performance index and constraints are considered. And finally the systematically optimized method is proposed.
Keywords
Optimization; Guidance and control system; Optimal problem formulation; Performance index; Constraints;
Citations & Related Records
Times Cited By KSCI : 2  (Citation Analysis)
연도 인용수 순위
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