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太阳敏感器与磁强计组合定姿及陀螺漂移估计算法

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针对磁强计或太阳敏感器仅能估计两轴姿态的问题,提出将太阳敏感器和磁强计测量信息作为观测量,通过与基于卫星轨道和姿态角速率推算的太阳指向和磁场强度比较,估计陀螺积分姿态推算误差,校正陀螺积分姿态,并基于PI滤波估计陀螺漂移.仿真试验结果表明姿态确定精度为1°左右.
Algorithm of Attitude Determination and Drift Estimation of Gyro Based on Sun Sensor and Magnetometer
Aiming at the problem that magnetometer or sun sensors can only estimate the attitude of two axes,the observed quantity is presented by using the method of taking advantage of the observation vector measured by sun sensors and magnetometer,the attitude error is gained by using sun vector which is com-pared with the geomagnetic field vector estimated based on the orbit and the attitude angular velocity of the satellite.The integrated attitude of the gyro is corrected by the attitude error estimated based on the sun vec-tor and the geomagnetic field vector,and the gyro drift is estimated based on PI filter.The simulation result shows that the attitude determination precision reaches about 1°.

GyroSun sensorMagnetometerIntegrated attitude determinationDrift estimationSatellite

王献忠、张肖

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上海市空间智能控制技术重点实验室,上海 201109

上海航天技术研究院,上海 201109

上海航天控制技术研究所,上海 201109

陀螺 太阳敏感器 磁强计 组合定姿 漂移估计 卫星

2024

航天控制
北京航天自动控制研究所

航天控制

CSTPCD
影响因子:0.29
ISSN:1006-3242
年,卷(期):2024.42(6)