助推持续导弹的最佳射程研究

1988 American Control Conference Pub Date : 1988-06-15 DOI:10.1109/ACC.1988.4172731

S. Katzir, E. Cliff, H. Kelley

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引用次数: 3

摘要

研究了一种具有持续推进力的空空导弹的中段制导。研究了以载荷因子为控制变量的垂直平面点质量模型。在开环条件下，通过通常的必要条件和多次射击算法计算时间-范围-能量最优轨迹。研究了终端速度大小对射击距离的影响。

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Best-Range Study for a Boost-Sustain Missile

Midcourse guidance is examined for an air-to-air missile featuring boost-sustain propulsion. A vertical plane, point-mass model is studied with load factor as a control variable. Time-range-energy optimal trajectories are computed, open-loop, via the usual necessary conditions and a multiple-shooting algorithm. A requirement on terminal velocity magnitude is examined for its effect on firing range.

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1988 American Control Conference

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