Autonomous attitude maneuver control method of deep space probe
A technology for deep space detectors and attitude maneuvering, which is applied in attitude control and other directions, and can solve problems such as shortening time
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[0066] A kind of autonomous attitude maneuver control method of deep space probe disclosed in this example, the specific implementation steps are as follows:
[0067] Step 1: Determine the vector of the sun in the inertial system as r according to the ephemeris time at the moment of attitude maneuver I =[1 0 0] T , and then determine the attitude transformation matrix from the inertial system to the detector body coordinate system as C BI = 0.4602 - 0.6354 0.6201 - 0.8786 - 0.4261 0.2156 0.1272 - 0.6440 ...
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