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Trajectory optimization for a missile with strap-down seeker against hypersonic target

机译:带有捷联导引头的高超声速目标导弹弹道优化

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Trajectory optimization against hypersonic ballistic target is performed for a missile with strap-down seeker. For successful interception, the hand-over point of the homing phase from midcourse phase should be properly determined, which is obtained by trajectory optimization in this study. Constraints on control inputs are introduced to consider the property of strap-down seeker. The direct method is used to solve the trajectory optimization problem. Numerical simulation is performed to demonstrate the performance of the proposed method.
机译:针对具有捷联式导引头的导弹,针对高超音速弹道目标进行弹道优化。为了成功拦截,应该适当地确定归零阶段从中途阶段的交接点,这是通过本研究中的轨迹优化获得的。引入了对控制输入的约束,以考虑捷联导引器的特性。直接法用于解决轨迹优化问题。数值模拟表明了该方法的有效性。

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