Satellite Attitude Estimation UKF Algorithm Based on Star-Sensor

机译：基于星敏感器的卫星姿态估计UKF算法

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The objective of this paper is to derive a satellite attitude estimation algorithm only using vector observation from the star-sensor, in gyros-less or gyro-disable mode. State estimation is achieved through the unscented Kalman filter (UKF) based on unscented transformation. Simulation results indicate that this approach is feasible and effective

机译：本文的目的是在无陀螺仪或陀螺仪禁用模式下，仅使用来自恒星传感器的矢量观测来推导卫星姿态估计算法。通过基于无味变换的无味卡尔曼滤波器（UKF）可以实现状态估计。仿真结果表明该方法是可行和有效的。

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《》|2006年|799-802|共4页
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Hui Li; Zhao-wei Sun; Shi-jie Zhang;
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Kalman filters; artificial satellites; attitude measurement; sensors; state estimation; satellite attitude estimation; star sensor; state estimation; unscented Kalman filter; vector observation; Attitude estimation; Starsensor; Unscented Kalman Filter; satellite;

机译：卡尔曼滤波器;人造卫星;姿态测量;传感器;状态估计;卫星姿态估计;星形传感器;状态估计;无味卡尔曼滤波器;矢量观测;姿态估计;星形传感器;无味卡尔曼滤波器;卫星;
入库时间 2022-08-26 15:15:25

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1. Research on GFSINS/Star-sensor Integrated Attitude Estimation Algorithm Based on UKF [J] . Minghong Zhu, Fei Yu, Shu Xiao, Engineering Letters . 2018,第4期

机译：基于UKF的GFSINS /星敏感器综合姿态估计算法研究
2. NANOSATELLITE ATTITUDE ESTIMATION FROM VECTOR MEASUREMENTS USING SVD-AIDED UKF ALGORITHM [J] . Demet Cilden, Halil Ersin Soken, Chingiz Hajiyev Metrology and Measurement Systems: Metrologia i Systemy Pomiarowe . 2017,第1期

机译：使用SVD辅助UKF算法从载体测量中纳米卫星姿态估计
3. REKF and RUKF for pico satellite attitude estimation in the presence of measurement faults [J] . Soken Halil Ersin, Hajiyev Chingiz Systems Engineering and Electronics, Journal of . 2014,第2期

机译：REKF和RUKF用于在存在测量故障的情况下微微卫星姿态估计
4. Satellite Attitude Estimation UKF Algorithm Based on Star-Sensor [C] . Hui Li, Zhao-wei Sun, Shi-jie Zhang . -1

机译：基于星敏感器的卫星姿态估计UKF算法
5. Development of novel satellite attitude determination and control algorithms based on telemetry data from an Earth satellite. [D] . Gollu, Narendra. 2008

机译：基于地球卫星遥测数据的新型卫星姿态确定和控制算法的开发。
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. Nanosatellite Attitude Estimation from Vector Measurements Using SVD-Aided UKF Algorithm [O] . Cilden Demet, Soken Halil Ersin, Hajiyev Chingiz 2017

机译：基于sVD辅助UKF算法的矢量测量纳米卫星姿态估计
8. Study of Design Methodologies for Digital Attitude Control System Algorithms. Volume 3: New Illustrative Concept Satellite (NICS), a Case Study in Attitude Control Subsystems (ADCS) Software Procurement [R] . Teule, F., Zwartbol, T., Slippens, C., 1982

机译：数字姿态控制系统算法设计方法研究。第3卷：新的说明性概念卫星（NICs），一个姿态控制子系统（aDCs）软件采购案例研究

Satellite Attitude Estimation UKF Algorithm Based on Star-Sensor

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