Fault tolerant control method for a spacecraft equipped with a flywheel based on robust adaptation
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- 陕西智星空间科技有限公司
- Publication Date
- 2015-09-02
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Abstract
Description
technical field
[0001] The invention relates to the technical field of spacecraft attitude control. Specifically, it relates to a robust adaptive-based fault-tolerant control method for spacecraft with flywheels. Using this method can ensure that the designed fault-tolerant control method can still effectively realize the attitude control of the spacecraft when there are external disturbances in the spacecraft and the reaction flywheel as the actuator has a torque loss failure. Background technique
[0002] Fault-tolerant control means that when some components in the control system fail, the system can still complete the control task safely under the condition that the expected performance index or performance index is slightly reduced (but acceptable). Research on fault-tolerant control makes it possible to improve the security and reliability of complex systems.
[0003] Fault Tolerant Control System (FTCS) can be divided into two categories: active fault tolerant contr...