A NOVEL-APPROACH TO THE ATTITUDE-CONTROL OF AXISYMMETRICAL SPACECRAFT

被引：95
作者：
TSIOTRAS, P [1 ]
CORLESS, M [1 ]
LONGUSKI, JM [1 ]
机构：
[1] PURDUE UNIV,SCH AERONAUT & ASTRONAUT,W LAFAYETTE,IN 47907
来源：
AUTOMATICA | 1995年 / 31卷 / 08期
关键词：
ATTITUDE CONTROL; STABILITY; NONLINEAR CONTROL SYSTEMS; FEEDBACK CONTROL;
D O I：
10.1016/0005-1098(95)00010-T
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
We consider the problem of attitude stabilization of an axisymmetric spacecraft using two pairs of gas jet actuators. These actuators provide control torques about two axes spanning the two-dimensional plane orthogonal to the axis of symmetry. Using a new kinematic formulation, we derive a stabilizing control law that achieves arbitrary reorientation of the spacecraft under the assumption that the initial spin rate about the symmetry axis is zero.
引用
收藏
页码：1099 / 1112
页数：14
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