Paper
1 December 2023 Control technology and verification of space advanced technology demonstration satellite
Author Affiliations +
Proceedings Volume 12940, Third International Conference on Control and Intelligent Robotics (ICCIR 2023); 1294008 (2023) https://doi.org/10.1117/12.3010650
Event: Third International Conference on Control and Intelligent Robotics (ICCIR 2023), 2023, Sipsongpanna, China
Abstract
Aiming at the requirement of low cost, high precision and high stability of space advanced technology demonstration satellite, a method of heterogeneous backup of attitude control sensor is proposed, and the design principle of the sensor is analyzed in depth multi-sensor information fusion algorithm is designed. The control strategy of the satellite is optimized, the weighted PID control strategy is designed, and a reasonable integral separation threshold is selected. Control bandwidth is adjusted to reduce the control deviation caused by time delay. The objective of the attitude control system is to achieve control accuracy better than 0.1°(3σ) and control stability better than 0.003°/s(3σ).Through the analysis of on-orbit test data, the control accuracy of the satellite is better than 0.005°(3σ), and the control stability is better than 0.0005°/s(3σ).
(2023) Published by SPIE. Downloading of the abstract is permitted for personal use only.
Jinsong Li, Yingquan Yang, Yonghe Zhang, Xiaofeng Zhang, Wen Chen, and Heng Zhou "Control technology and verification of space advanced technology demonstration satellite", Proc. SPIE 12940, Third International Conference on Control and Intelligent Robotics (ICCIR 2023), 1294008 (1 December 2023); https://doi.org/10.1117/12.3010650
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KEYWORDS
Satellites

Control systems

Bismuth

Angular velocity

Gyroscopes

Information fusion

Aerospace engineering

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