Integrated design and accuracy analysis of star sensor and gyro on the same benchmark for satellite attitude determination system

Bowen Hou; Zhangming He; Haiyin Zhou; Jiongqi Wang

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Integrated design and accuracy analysis of star sensor and gyro on the same benchmark for satellite attitude determination system

机译：卫星姿态确定系统在同一基准上的恒星传感器和陀螺仪的集成设计和精度分析

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As an important sensor in the navigation systems, star sensors and the gyro play important roles in spacecraft attitude determination system. Complex environmental factors are the main sources of error in attitude determination. The error influence of dif

机译：作为导航系统中的重要传感器，星形传感器和陀螺仪在航天器姿态确定系统中起着重要作用。复杂的环境因素是姿态确定中错误的主要来源。 dif的错误影响

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来源
《Automatica Sinica, IEEE/CAA Journal of》 |2019年第4期|1074-1080|共7页
作者
Bowen Hou; Zhangming He; Haiyin Zhou; Jiongqi Wang;
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作者单位

College of Liberal Arts and Science National University of Defense Technology Changsha 410072 China;

College of Liberal Arts and Science National University of Defense Technology Changsha 410072 China and also with Beijing Institute of Control Engine;

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正文语种 eng
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专利

1. Integrated Design and Accuracy Analysis of Star Sensor and Gyro on the Same Benchmark for Satellite Attitude Determination System [J] . Bowen Hou, Zhangming He, Haiyin Zhou, 自动化学报（英文版） . 2019,第004期

机译：卫星姿态确定系统在同一基准下星型传感器和陀螺仪的集成设计和精度分析
2. Integrated Design and Accuracy Analysis of Star Sensor and Gyro on the Same Benchmark for Satellite Attitude Determination System [J] . Bowen Hou, Zhangming He, Haiyin Zhou, 自动化学报：英文版 . 2019,第004期

机译：卫星姿态确定系统在同一基准下星型传感器和陀螺仪的集成设计和精度分析
3. Design on a Multi-Sensor Integrated Attitude Determination System for Small UAVs [J] . Cun-Xiao Miao, Juan-Juan Cao, Jian-Cheng Fang 哈尔滨工业大学学报（英文版） . 2014,第006期

机译：小型无人机多传感器综合姿态确定系统设计
4. Gyro / Star Tracker Integration for Satellite High-Accuracy Attitude Determination Considering Relative Sensor Kinematics [C] . S. Winkler, G. Wiedermann, W. Gockel Symposium gyro technology . 2008

机译：陀螺/星跟踪器集成，用于考虑相对传感器运动学的卫星高精度姿态确定
5. Design, analysis, implementation and testing of the thermal control, and attitude determination and control systems for the CanX-7 nanosatellite mission. [D] . Cotten, Bradley Scott. 2014

机译：用于CanX-7纳米卫星任务的热控制以及姿态确定和控制系统的设计，分析，实施和测试。
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. Fast Converging with High Accuracy Est imates of Satellite Attitude and Orbit Based on Magnetometer Augmented with Gyro, Star Sensor and GPS via Extended Kalman Filter [O] . T. Habib 2019

机译：快速收敛于高精度EST型卫星姿态和轨道基于磁力计的轨道，通过扩展卡尔曼滤波器增强了陀螺仪，星形传感器和GPS

Integrated design and accuracy analysis of star sensor and gyro on the same benchmark for satellite attitude determination system

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