摆动地球敏感器,探测器,姿态,地球同步轨道卫星, ," /> 摆动地球敏感器,探测器,姿态,地球同步轨道卫星, ,"/> swing earth sensor,bolometer detector,attitude,geostationary satellite,

 , ,"/> <span style="font-size:10.5pt;font-family:宋体;">利用摆动地球敏感器两个探测器输出的姿态确定</span><span style="font-size:medium;"></span>

中国科技核心期刊

中文核心期刊

CSCD来源期刊

空间控制技术与应用 ›› 2008, Vol. 34 ›› Issue (2): 14-17.

• 论文与报告 • 上一篇    下一篇

利用摆动地球敏感器两个探测器输出的姿态确定

  

  1. 北京控制工程研究所
  • 出版日期:2008-04-25 发布日期:2021-12-11

Spacecraft Attitude Determination Using Two Detectors of Swing Earth Sensor

  1. Beijing institute of Control Engineering
  • Online:2008-04-25 Published:2021-12-11

摘要:

摆动地球敏感器是地球同步通信卫星控制系统的重要部件。这种敏感器主要用于卫星的姿态测量, 测量量作为控制系统的输入信号计算控制输出量。摆动地球敏感器有4个探测器, 目前在轨卫星的基本使用方法均为至少使用3个探测器的测量信息进行姿态确定。本文给出了使用2个探测器测量确定卫星姿态的计算方法, 并结合实际情况给出了使用策略。这种姿态确定方法大大拓宽了地球敏感器的使用范围, 增加了地球敏感器的冗余性, 延长了部件的使用寿命。

关键词:

font-size:10.5pt, font-family:Calibri, sans-serif, "> ">摆动地球敏感器">摆动地球敏感器sfield=kw&, skey=%E6%91%86%E5%8A%A8%E5%9C%B0%E7%90%83%E6%95%8F%E6%84%9F%E5%99%A8&, code=&, ')">uid=WEEvREcwSlJHSldTTEYzVDhUQ01wZWNBc3JTenlNbHhvcDE3MXFEZWxwQT0=$9A4hF_YAuvQ5obgVAqNKPCYcEjKensW4IQMovwHtwkF4VYPoHbKxJw!!" target="https://kns.cnki.net/KXReader/_blank">, color:windowtext, 探测器">探测器sfield=kw&, skey=%E6%8E%A2%E6%B5%8B%E5%99%A8&, code=&, ')">uid=WEEvREcwSlJHSldTTEYzVDhUQ01wZWNBc3JTenlNbHhvcDE3MXFEZWxwQT0=$9A4hF_YAuvQ5obgVAqNKPCYcEjKensW4IQMovwHtwkF4VYPoHbKxJw!!" target="https://kns.cnki.net/KXReader/_blank">, color:windowtext, 姿态">姿态sfield=kw&, skey=%E5%A7%BF%E6%80%81&, code=&, ')">uid=WEEvREcwSlJHSldTTEYzVDhUQ01wZWNBc3JTenlNbHhvcDE3MXFEZWxwQT0=$9A4hF_YAuvQ5obgVAqNKPCYcEjKensW4IQMovwHtwkF4VYPoHbKxJw!!" target="https://kns.cnki.net/KXReader/_blank">, color:windowtext, 地球同步轨道卫星">地球同步轨道卫星sfield=kw&, skey=%E5%9C%B0%E7%90%83%E5%90%8C%E6%AD%A5%E8%BD%A8%E9%81%93%E5%8D%AB%E6%98%9F&, code=&, ')">uid=WEEvREcwSlJHSldTTEYzVDhUQ01wZWNBc3JTenlNbHhvcDE3MXFEZWxwQT0=$9A4hF_YAuvQ5obgVAqNKPCYcEjKensW4IQMovwHtwkF4VYPoHbKxJw!!" target="https://kns.cnki.net/KXReader/_blank">,

Abstract:

The digital infrared earth sensor (IRES) is an important component of the geostationary earth orbit (GEO) satellite control system.IRES is used to measure the satellite attitude.Its outputs are used to compute the control torques for satellites.The IRES have four bolometer detectors.The attitude of any Chinese GEO satellite in orbit is determined using the information of three bolometer detectors at least.This paper develops an attitude determination method using two bolometer detectors only and gives an application strategy based on the real situation.With this method, the IRES application range is expanded, the redundancy is enhanced, and the lifetime is increased.

Key words:

font-size:10.5pt, font-family:Calibri, sans-serif, "> color:windowtext, swing earth sensor">swing earth sensorsfield=kw&, skey=swing%20earth%20sensor, bolometer%20detector, attitude, geostationary%20satellite&, code=&, ')">uid=WEEvREcwSlJHSldTTEYzVDhUQ01wZWNBc3JTenlNbHhvcDE3MXFEZWxwQT0=$9A4hF_YAuvQ5obgVAqNKPCYcEjKensW4IQMovwHtwkF4VYPoHbKxJw!!" target="https://kns.cnki.net/KXReader/_blank">, bolometer detector, attitudesfield=kw&, skey=swing%20earth%20sensor, bolometer%20detector, attitude, geostationary%20satellite&, code=&, ')">uid=WEEvREcwSlJHSldTTEYzVDhUQ01wZWNBc3JTenlNbHhvcDE3MXFEZWxwQT0=$9A4hF_YAuvQ5obgVAqNKPCYcEjKensW4IQMovwHtwkF4VYPoHbKxJw!!" target="https://kns.cnki.net/KXReader/_blank">, geostationary satellitesfield=kw&, skey=swing%20earth%20sensor, bolometer%20detector, attitude, geostationary%20satellite&, code=&, ')">uid=WEEvREcwSlJHSldTTEYzVDhUQ01wZWNBc3JTenlNbHhvcDE3MXFEZWxwQT0=$9A4hF_YAuvQ5obgVAqNKPCYcEjKensW4IQMovwHtwkF4VYPoHbKxJw!!" target="https://kns.cnki.net/KXReader/_blank">,

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中图分类号: 

  • TN215