固体火箭技术2012，Vol.35Issue(1)：17-23,7.
基于固体微推力器阵列的卫星控制一体化算法
Integrated control algorithm based on solid propellant micro-thruster array
摘要
Abstract
In order to make solid propellant micro-thruster array more practical,the layout method which can be used in attitude and orbit control was proposed. The mathematical model of allocation algorithm was established and the concept was introduced to ensure that the least thrusters were used. The dynamic programming and the greedy strategy were introduced into the problem and the solving mathematical model was established. Through analysis and simulation, this method can effectively solve the problem, which is conductive to achieve real-time control.关键词
固体微型推力器阵列/推力器布局/分配算法/阵列规划算法/实时控制Key words
solid propellant micro-thruster array/thrusters layout/allocation algorithm/array programming algorithm/real-time control分类
航空航天引用本文复制引用
刘旭辉,方蜀州,马红鹏,高庆丰..基于固体微推力器阵列的卫星控制一体化算法[J].固体火箭技术,2012,35(1):17-23,7.基金项目
“十一五”民用航天科研预先研究项目——微型推力器阵列技术(C2220062202). （C2220062202）
