Attitude control feedback loop based on combined fixed attitude of multi-rate sensor
Patent Information
- Authority / Receiving Office
- CN · China
- Current Assignee / Owner
- BEIHANG UNIV
- Publication Date
- 2011-07-06
- Estimated Expiration
- Not applicable · inactive patent
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Abstract
Description
technical field
[0001] The invention relates to an attitude control feedback loop based on multi-rate sensor combination attitude determination, which belongs to the field of spacecraft attitude determination. Background technique
[0002] As the main means of space environment detection, satellite technology research is particularly important, and all countries have invested a lot of manpower and material resources in research. With the development of aerospace science and technology, satellites have higher and higher requirements for attitude stability, pointing or maneuvering control capabilities, system functions are becoming more and more complex, longer operating life is required, and the efficiency of satellites is getting higher and higher. ability. Generally speaking, multi-task, high-precision, long-life, and high-reliability satellites have become a new development trend.
[0003] One of the most important technologies in the satellite system is the design of th...