利用摆动地球敏感器两个探测器输出的姿态确定

Abstract

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:

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CLC Number:

TN215

LIU Xinyan.

Spacecraft Attitude Determination Using Two Detectors of Swing Earth Sensor [J].Aerospace Contrd and Application, 2008, 34(2): 14-17.

0
/ / Recommend swing earth sensor;bolometer detector;attitude;geostationary satellite;

”. Please open it by linking:http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/abstract/abstract9390.shtml" name="neirong"> swing earth sensor;bolometer detector;attitude;geostationary satellite;

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Spacecraft Attitude Determination Using Two Detectors of Swing Earth Sensor

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