| 摆动扫描地球敏感器数学模型及飞行试验结果 |
| |
| 引用本文： | 孙宝祥,赵健翔,李宝绶.摆动扫描地球敏感器数学模型及飞行试验结果[J].航天控制,2000,18(2):40-45. |
| |
| 作者姓名： | 孙宝祥 赵健翔 李宝绶 |
| |
| 作者单位： | 北京控制工程研究所!北京100080 |
| |
| 摘 要： | 描述了东方红三号卫星(DFH-3)控制系统设计和数学仿真中采用的摆动扫描地球敏感器IRES-01的数学模型，东方红三号卫星近三年飞行试验结果与数学仿真结果基本一致，证明数学模型是正确的。
|
| 关 键 词： | 地球敏感器 数学模型 飞行试验 |
| 修稿时间： | 1999-12-01 |
The Mathematical Model and the Flight Results of the Swing Scanning Earth Sensor |
| |
| Sun Baoxiang
,Zhao Jianxiang
,Li Baoshou.The Mathematical Model and the Flight Results of the Swing Scanning Earth Sensor[J].Aerospace Control,2000,18(2):40-45. |
| |
| Authors: | Sun Baoxiang Zhao Jianxiang Li Baoshou |
| |
| Institution: | Sun Baoxiang
,Zhao Jianxiang
,Li Baoshou
(Beijing Institute of Control Engineering, Beijing 100080) |
| |
| Abstract: | The paper describes the mathematical model of the swing scanning earth sensor IRES-01 used in design and mathematical simulation of DFH-3 satellite control system.During 3 years the flight results of DFH-3 Satellite is coincident with the results of the mathematical simulation, showing that the mathematical model is correct. |
| |
| Keywords: | Earth sensor Mathematical model Flight test |
| 本文献已被 CNKI 万方数据 等数据库收录！ |
