제어로봇시스템학회:학술대회논문집

제어로봇시스템학회 (Institute of Control, Robotics and Systems)
권호 표지

최적유도법칙의 closed-form 해와 근사식

The closed-form solution and its approximation of the optimal guidance law

  • 탁민제 (한국과학기술원 항공우주공학과) ;
  • 박봉규 (한국과학기술원 항공우주공학과) ;
  • 선병찬 (한국과학기술원 항공우주공학과) ;
  • 황인석 (한국과학기술원 항공우주공학과) ;
  • 조항주 (국방과학연구소) ;
  • 송택렬 (국방과학연구소)
  • 발행 : 1992.10.01
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초록

In this paper, the optimal homing guidance problem is investigated for the general missile/target models described in the state-space. The closed-form solution of the optimal guidance law derived, and its asymptotic properties are studied as the time-to-go goes to infinity or zero. Futhermore, several approximate solutions of the optimal guidance law are suggested for real-time applications.

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