Diagnosability determining method of satellite control system based on transfer functions
A satellite control system and transfer function technology, applied in the aerospace field, can solve the problems of lack of pertinence, feedback impact, and only applicable
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specific Embodiment approach
[0066] ①Satellite attitude dynamics and kinematic equations
[0067] The satellite attitude dynamic equation based on the body coordinate system is:
[0068] I x ω · x - ( I y - I z ) ω y ω z = u x
[0069] I y ω · y - ( I z - I x ) ω z ω x = u y - - ...
Embodiment approach
[0101] According to the fault model of the satellite control system in step (1), the obtained sensor fault-to-output transfer function is:
[0102] T f s , i = F s , i D k F s , i + C 0 D k C C ...
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