Assembly spacecraft closed loop feedback optimal control distribution method
A technology of optimal control and distribution method, applied in attitude control, non-electric variable control, control/regulation system, etc., can solve problems such as control accuracy reduction and installation error
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[0040] like figure 2 As shown, the specific implementation steps of the present invention are as follows (the following is an example to illustrate the specific implementation of the method by taking the composite spacecraft formed by the abandoned micro-satellite and service satellite in space):
[0041] The first step is to establish the attitude kinematics and dynamics models of the abandoned micro-satellites and service satellites:
[0042] q · = 1 2 ( q 0 ω + q × ω ) q · 0 = - ...
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