1. Research on Interference Identification and Compensation Method of Periodic Rotating Payload of Satellite
- Author
-
Nie Zhanghai, Bai Jiaxiang, Cheng Zhaoyang, and Peng Rui
- Subjects
Angular momentum ,Payload ,Computer science ,Control theory ,Orbit (dynamics) ,Torque ,Angular velocity ,Satellite ,Rotation ,Reaction wheel - Abstract
When a satellite equipped with large angular momentum rotational payload is in orbit for a long time, the angular momentum generated by the detection head of the rotational payload is mainly compensated by the attitude and orbit control system, the rotation characteristic will directly affect the satellite attitude stability. When the rotation characteristic of the detection head deviates greatly from the design index, it will affect the attitude stability of the satellite and cause the attitude of the satellite to be unstable. Based on the analysis of on-orbit data, in order to suppress the rotation characteristics of the payload detection head, the paper designed a method for feedforward compensation using reaction wheel. Finally, through on-orbit tests and data analysis, the validity and practicability of the design algorithm are verified.
- Published
- 2020