| 离散相似法在卫星姿态控制系统设计和数字仿真中的应用 |
| |
| 引用本文： | 周文忠,李果.离散相似法在卫星姿态控制系统设计和数字仿真中的应用[J].航天控制,1994(1). |
| |
| 作者姓名： | 周文忠 李果 |
| |
| 作者单位： | 北京控制工程研究所 |
| |
| 摘 要： | 本文叙述了离散相似法的基本原理，在此基础上给出了单输入－单输出系统的各种典型子块的系数计算公式，在典型子块的基础上构成晃动动力学、帆板挠性动力学、双二阶晃动和帆板振动滤波器动力学的复合子块，以及各种非线性复合子块。最后给出了某卫星三轴姿态控制系统的数字仿真结果。
|
| 关 键 词： | 离散相似法，卫星姿态控制系统，系统仿真 |
An application of Discrete Similarity Method in the Design and Digital Simulation for Satellite Attitude Control System |
| |
| Zhou Wenzhong, Li Guo.An application of Discrete Similarity Method in the Design and Digital Simulation for Satellite Attitude Control System[J].Aerospace Control,1994(1). |
| |
| Authors: | Zhou Wenzhong Li Guo |
| |
| Institution: | Beijing Institute of Control Engineering |
| |
| Abstract: | Based on the basic concept of Discrete Similarity Method descirbed in this paper, the coefficients of expressions of typical blocks for single input/single output systems have been derived. Complex blocks such as sloshing dynamics, flexible array dynamics, double two-order sloshing and vibration filter dynamics and various non-linear blocks can be constructed by employing a combination of typical blocks. Finally, the digital simulation for a three-axis stabilized attitude control system of a satellite has been given. |
| |
| Keywords: | Discrete similarity method Satellite attitude control system System simulation |
| 本文献已被 CNKI 等数据库收录！ |
