Optimal scheme selection method for satellite control system on basis of reconfigurable constraints of failures
A satellite control system and a technology for scheme optimization, applied in the aerospace field, can solve the problem of not considering the configuration of each component of the system, etc.
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[0101] For satellite control systems, summarize commonly used sensor and actuator configurations. Sensors typically include gyroscopes, star sensors, infrared earth sensors, and sun sensors. Actuators typically include momentum wheels, control torque gyros, propulsion systems, and magnetic torque device. According to the task requirements, the optional configuration of the executor is set as a={a 1 ,a 2 ,...,a m}, the optional sensor configuration is s={s 1 ,s 2 ,...,s p}. In steady state, the system can be described by the following linear system:
[0102] x · ( t ) = Ax ( t ) + Bu ( ...
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