Ignition algorithm of solid propellant micro-thruster array for attitude control

LIU Xu-hui; FANG Shu-zhou; LIU Shu-jie; LUO Li; QUAN En

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Ignition algorithm of solid propellant micro-thruster array for attitude control

更新时间：2026-07-07

- Ignition algorithm of solid propellant micro-thruster array for attitude control
- Vol. 26, Issue 7, (2011)
- 作者机构：
  
  1. 北京理工大学宇航学院,北京,100081
  2. 中国航天科技集团公司中国空间技术研究院北京控制工程研究所,北京,100190
- 作者简介：
- 基金信息：
- DOI：
  CLC：
- Published：2011
- 稿件说明：
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LIU Xu-hui, FANG Shu-zhou, LIU Shu-jie, et al. Ignition algorithm of solid propellant micro-thruster array for attitude control[J]. 2011, 26(7).
DOI：

LIU Xu-hui, FANG Shu-zhou, LIU Shu-jie, et al. Ignition algorithm of solid propellant micro-thruster array for attitude control[J]. 2011, 26(7). DOI：

摘要

对用于微型卫星姿态控制的固体推力器阵列的组合点火问题进行了研究

分析了微型固体推力器阵列的工作性能

建立了组合点火问题的数学模型

设计了基值组合算法和阵列规划算法两种点火算法

并利用Matlab/Simulink对设计的算法进行了仿真.结果表明:阵列规划算法计算准确

快速有效

并且提高了阵列中推力器的利用率.

Abstract

The study on ignition algorithm of solid propellant micro-thruster array for attitude control of micro-satellite was made and described in this paper.The performance capabilities of solid propellant micro-thruster array were analyzed and the theoretical model was set up

then two kinds of ignition algorithms

that were combined base value algorithm and array programming algorithm

were proposed and verified by simulation using Matlab/Simulink.The simulation shows that

array programming algorithm is accurate and fast

also can improve the utilization efficiency of thrusters in the array.

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Related Author

Haisen YU

Shujun TAN

Zhigang WU

WANG Xiao-feng

HUANG Hai

QIN Li

YANG Ming

GUO Qing

Related Institution

State Key Laboratory of Structural Analysis for Industrial Equipment，Dalian University of Technology

Key Laboratory of Advanced Technology for Aerospace Vehicles，Liaoning Province，Dalian University of Technology

School of Astronautics, Beijing University of Aeronautics and Astronautics

Control and Simulation Center, Harbin Institute of Technology

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