Aiming at satellite attitude system which is composed of gyroscopes, infrared earth sensors and solar sensors, we set up the model of the satellite attitude detemination by using quaternion, and build kalman filter for information fusion. The simulation result indicates that this method can provide satellite attitude parameters which satisfy the requirement.
参考文献
相似文献
引证文献
引用本文
刘志俭,吴美平,胡小平.多敏感器卫星姿态确定的卡尔曼滤波器设计[J].国防科技大学学报,2001,23(6):28-32. LIU Zhijian, WU Meiping, HU Xiaoping. Kalman Filter Design for Multi-sensors Satellite Attitude Determination[J]. Journal of National University of Defense Technology,2001,23(6):28-32.