제어로봇시스템학회:학술대회논문집
- 1992.10a
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- Pages.572-577
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- 1992
The closed-form solution and its approximation of the optimal guidance law
최적유도법칙의 closed-form 해와 근사식
Abstract
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.