Title :
A modified CLOS guidance law via right inversion
Author :
Huang, Jie ; Lin, Ching Fang
Author_Institution :
American GNC Corp., Chatsworth, CA, USA
fDate :
29 June-1 July 1994
Abstract :
The CLOS guidance law of Ha and Chong (1992) via feedback linearization is modified. The original nonlinear tracking problem is simplified to a right inversion problem for a linear time-varying system. Moreover, an assumption of Ha and Chong is eliminated by making use of the orthogonal property of a rotational matrix.
Keywords :
feedback; linearisation techniques; missile guidance; feedback linearization; linear time-varying system; missile guidance; modified CLOS guidance law; nonlinear tracking problem; orthogonality; right inversion; right inversion problem; rotational matrix; Acceleration; Computer simulation; Feedback; Geometry; Missiles; Target tracking;
Conference_Titel :
American Control Conference, 1994
Print_ISBN :
0-7803-1783-1
DOI :
10.1109/ACC.1994.735185
