Reachable Set Control For Preferred Axis Homing Missiles

D. Caughlin, T. Bullock
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引用次数: 5

Abstract

This paper presents the results of a linear control technique developed for fixed-final-time constrained systems and applied to preferred axis homing missiles. This technique accommodated the nonlinearities, constraints, and the modeling errors of a suboptimal linear design to maintain the target within the missile reachable set. This feature minimized miss distances, and prevented control saturation during the terminal portion of the trajectory.
首选轴制导导弹的可达设定控制
本文介绍了一种用于固定最终时间约束系统的线性控制技术,并将其应用于优选轴寻的导弹。该方法考虑了非线性、约束和次优线性设计的建模误差,使目标保持在导弹可达集中。这一特点最大限度地减少了脱靶距离,并防止在弹道的末端部分控制饱和。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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