Satellite attitude control method for ground point staring imaging
A satellite attitude control and gaze imaging technology, applied in attitude control and other directions, can solve the problems of complex algorithms, verified, and satellite gaze attitude control methods remain at the theoretical level, etc.
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[0078] Hereinafter, the present invention will be further described in detail with reference to specific embodiments and the drawings of the specification.
[0079] A satellite attitude control method for staring and imaging the ground point, the specific steps are as follows:
[0080] Step 1: Given satellite orbit state X S =[R S ,V S ] And the ground point space coordinate R T
[0081] R S =[1590360.821,6167656.906,2550832.279] T (m)
[0082] V S =[1712.222,2465.737,-7003.521] T (m / s)
[0083] R T =[1660202.218,5739273.073,2225233.992] T (m)
[0084] Where R S Is the position of the satellite's geocentric inertial system, V S Is the satellite’s geocentric inertial system velocity, R T Is the geocentric inertial system position of the ground point.
[0085] Step 2: Calculate the amount of error between the actual angular velocity and the desired angular velocity
[0086] 1) Calculate the gaze Euler angle
[0087] Calculate the normal unit vector of the satellite orbit surface at the curren...
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