伪控制策略的扩展,应用于特征结构分配偏航指向/横向平移控制律

K. Sobel, E. Shapiro
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引用次数: 3

摘要

K.M.索贝尔和F.J.拉曼(《指南杂志》)。, control . and Dyn., vol.12, no。针对飞行推进控制耦合飞机的线性化横向动力学,采用特征结构分配方法设计了偏航指向/横向平移控制器。作者提出了Sobel和Lallman给出的伪控制策略的扩展,该策略允许设计者通过调整一个以alpha表示的二维参数向量来权衡横向平移响应中的耦合与较小的奇异值(I+FG)的最小值。当α为零矢量时,新的可调策略简化为Sobel和Lallman所示的伪控制。利用伪控制策略的新扩展,提出了一种新的偏航指向/横向平移特征结构分配控制器。伪控制策略的扩展表明,当使用特征结构分配时,允许设计者自由地权衡鲁棒性和偏航指向解耦。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
An extension to the pseudo control strategy with application to an eigenstructure assignment yaw pointing/lateral translation control law
K.M. Sobel and F.J. Lallman (Journal of Guid., Contr., and Dyn., vol.12, no.3 pp.318-324, May-Jun, 1989) used eigenstructure assignment to design a yaw pointing/lateral translation controller for the linearized lateral dynamics of the flight propulsion control coupling aircraft. The authors propose an extension to the pseudo control strategy given by Sobel and Lallman which allows the designer to trade off the coupling in the lateral translational response with the minimum of the smaller singular value of (I+FG) by adjusting a two-dimensional parameter vector denoted by alpha . When alpha is the zero vector, then the new adjustable strategy reduces to the pseudo control shown by Sobel and Lallman. A new yaw pointing/lateral translation eigenstructure assignment controller is presented, which uses the new extension to the pseudo control strategy. The extension to the pseudo control strategy is shown to allow the designer freedom in trading off robustness and yaw pointing decoupling when using eigenstructure assignment.<>
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