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Spacecraft Integrated Attitude Determination Based on GPS/IMU/Sun Sensor
Author(s): 
Pages: 7-13
Year: Issue:  3
Journal: AEROSPACE CONTROL

Keyword:  全球定位系统*姿态确定空间飞行器卡尔曼滤波;
Abstract: GPS定姿是GPS在空间飞行器上应用的一个重要方向,本文在建立GPS/惯性组件/太阳敏感器组合定姿系统的非线性模型的基础上,采用扩展卡尔曼滤波实现了该组合定姿方案.通过理论分析和仿真结果均验证了方案的可行性.为GPS定姿在空间飞行器的实际应用提供一定的参考.
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