A MODIFIED CLOS GUIDANCE LAW VIA RIGHT INVERSION

被引：13

作者：

HUANG, J

LIN, CF

机构：

[1] American GNC Corporation, Canoga Park, CA 91304

来源：

IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS | 1995年 / 31卷 / 01期

关键词：

D O I：

10.1109/7.366334

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

A command to line-of-sight (CLOS) guidance law is derived via right inversion. This CLOS guidance law achieves the same objective as that given by Ha and Chong via feedback linearization [1] yet is considerably simpler than that in [1] and does not rely on [1, Assumption 3]. These advantages are made possible by reformulating the original nonlinear tracking Problem as a right inversion problem for a linear time-varying system, and by making use of the orthogonal property of a rotational matrix.

引用

页码：491 / 495

页数：5