Around moon satellite dual spindle antenna direct land control method
A pointing control and antenna pair technology, which is applied to antennas suitable for movable objects, guidance devices for space navigation vehicles, etc., can solve problems such as complex control logic, and achieve the effect of simplifying the calculation process and ensuring accuracy.
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[0020] As shown in FIG. 1 , the flow chart of the dual-axis antenna pointing control of the present invention, the specific steps are as follows:
[0021] (1) First inject t into the star on the ground 0 (t 0 It can be the ephemeris information of the earth at any time corresponding to the ephemeris information that has been calculated on the ground, and the ephemeris of the earth in the equatorial inertial system at any time t is calculated according to the extrapolation algorithm. The vector E of the moon's center pointing to the earth's center in the moon-center equatorial inertial frame i Calculation formula:
[0022] u e = u l 0 + u l 0 · ( t - t 0 ) ...
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