Research on Satellite Attitude Determination with Adaptive Filter

机译：自适应滤波器卫星姿态测定研究

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When satellite is running, it may be influenced by external factors, and the measurement models of gyro and star sensor are changing with time uncertainly. This situation may lead extended Kalman filter(EKF) divergent. So new adaptive filter can be used in this situation, and it can estimate process noise and measuring noise on-time. This paper has applied Sage-Husa adaptive filter in satellite attitude determination. This adaptive filter algorithm can estimate satellite attitude parameters and gyro drift on-time with high accuracy reaching 10~(-3) level, and stability of the algorithm is also very good.

机译：当卫星正在运行时，可能受到外部因素的影响，并且陀螺仪和星传感器的测量模型在不确定的时间内随时间变化。这种情况可能导致扩展卡尔曼滤波器（EKF）发散。因此，可以在这种情况下使用新的自适应滤波器，并且它可以估算过程噪声和准时测量噪声。本文在卫星姿态确定中施加了Sage-Husa自适应滤波器。这种自适应滤波算法可以估计卫星姿态参数和陀螺仪，随着10〜（-3）水平的高精度，算法的稳定性也非常好。

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《IEEE International Conference on Information and Automation》|2010年||共4页
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作者
Lin Zhao; Chen Huang; Xinzhe Wang; Zhonghua Su;
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中图分类 TP2-53;
关键词
Sage-Husa adaptive filter; EKF; Gyro; Star sensor;

机译：Sage-Husa自适应过滤器;EKF;Gyro;星传感器;

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专利

1. ATTITUDE AND BIAS DETERMINATION USING ADAPTIVE UNSCENTED KALMAN FILTERING FOR ESMO SATELLITE [J] . Claudiu-Lucian PRIOROC, Raluca Mihaela STEFANESCU, Adrian Mihail STOICA University Politechnica of Bucharest scientific bulletin, D. Mechanical Engineering . 2013,第1期

机译：使用ESMO卫星的自适应无味卡尔曼滤波进行姿态和偏置确定
2. A residual based adaptive unscented Kalman filter for fault recovery in attitude determination system of microsatellites [J] . Huy Xuan Le, Saburo Matunaga Acta astronautica . 2014,第1期

机译：基于残差的自适应无味卡尔曼滤波器在微卫星姿态确定系统中的故障恢复
3. Adaptive Square-Root Cubature-Quadrature Kalman Particle Filter for satellite attitude determination using vector observations [J] . Maryam Kiani, Seid H. Pourtakdoust Acta astronautica . 2014,第1期

机译：基于矢量观测的自适应平方根Cubature正交卡尔曼粒子滤波器用于卫星姿态确定
4. ADAPTIVE KALMAN FILTERING ALGORITHM FOR SMALL SATELLITE ATTITUDE DETERMINATION BY USING GPS/GYRO INTEGRATED SYSTEM [C] . Jianjun Luo, Jianping Yuan, Junwu Wang, 52nd International Astronautical Congress Oct 1-5, 2001 Toulouse, France . 2001

机译：GPS /陀螺仪集成系统的自适应卡尔曼滤波算法在小卫星姿态确定中的应用
5. FILTERING THEORY METHODS AND APPLICATIONS TO THE ORBIT DETERMINATION PROBLEM FOR NEAR-EARTH SATELLITES. [D] . MYERS, KENNETH ALAN. 1974

机译：近地卫星轨道确定问题的滤波理论方法和应用。
6. QMRPF-UKF Master-Slave Filtering for the Attitude Determination of Micro-Nano Satellites Using Gyro and Magnetometer [O] . Peiling Cui, Huijuan Zhang 2010

机译：使用陀螺仪和磁力计确定微纳卫星姿态的QMRPF-UKF主从滤波
7. QMRPF-UKF Master-Slave Filtering for the Attitude Determination of Micro-Nano Satellites Using Gyro and Magnetometer [O] . Cui, Peiling, Zhang, Huijuan 2010

机译：使用陀螺仪和磁力计确定微纳卫星姿态的QMRPF-UKF主从滤波
8. Attitude determination using an adaptive multiple model filtering Scheme [R] . Lam, Quang, Ray, Surendra N. 1995

机译：使用自适应多模型过滤方案确定姿态

Research on Satellite Attitude Determination with Adaptive Filter

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