Time-optimal control application for an exoatmospheric interceptor

S.D. Cragon
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Abstract

The optimum control solution for the capture of an exoatmospheric interceptor's attitude and rate errors is derived. A practical application of the method is investigated by considering the timing constraints imposed by the pulsewidth modulation scheme, and, as a result, timing logic for the thruster firings is derived. The concept is verified by comparing a three-pulse capture with the optimum two-pulse capture and the two-pulse capture with wait time using a 6-DOF simulation of an exoatmospheric interceptor. This comparison demonstrates a considerable improvement in the response time of the control.<>
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大气层外拦截弹的时间最优控制应用
导出了捕获大气层外拦截器姿态和速率误差的最优控制解。通过考虑脉宽调制方案所施加的时序约束,研究了该方法的实际应用,并推导了推力器点火的时序逻辑。通过比较三脉冲捕获与最佳双脉冲捕获以及双脉冲捕获与等待时间,利用大气层外拦截器的六自由度模拟验证了该概念。这一对比表明,控制的响应时间有了相当大的改善。
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