一类卫星推力器布局的多目标优化设计方法  

A Multi-Objective Optimization Method of Thruster Configuration for a Class of Satellite

作　　者：林波[1,2] 武云丽[1,2] 

机构地区：[1]北京控制工程研究所,北京100190 [2]空间智能控制技术国家级重点实验室,北京100190

出　　处：《空间控制技术与应用》2010年第4期31-35,41,共6页Aerospace Control and Application

摘　　要：针对一类卫星平台的推力器布局进行优化方法建模,给出推力器布局设计原则和优化指标,将推力器布局问题转化为一个多约束多目标寻优问题.最后对IntelSat-VII/VIIA推力器布局进行优化设计,优化结果达到了预期效果,验证了本文方法和指标的有效性.A multi-objective optimization method for thrusters configuration is proposed for a class of satellites. In the paper, several optimization goals and design criterion are given for positioning and orienting thrusters. The position and the orientation of thrusters are achieved by solving the multi-objective optimization problem. Finally, the method is used to achieve positioning and oriening of thrusters for IntelSat- VII/VIIA, the results show the method is valid.

关 键 词：推力器布局 姿态控制 航天器 布局优化 

分 类 号：V448[航空宇航科学与技术—飞行器设计]