Moon landing satellite formation initialization method
An initialization method and satellite formation technology, which are applied in the field of satellite formation initialization and satellite formation in the moon-going moon, and can solve the problems of difficult application of satellite formations.
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[0063] The present embodiment discloses a method for initializing a satellite formation to the moon, establishing satellite dynamic equations in the inertial systems of the earth and the moon respectively; through multiple multi-target orbit corrections, it is ensured that multiple satellites realize formation initialization. By adding midway correction during the earth-moon transfer, ensure that the orbital inclination of each satellite is the same, and the height of the perigee point is the same, and the time of reaching the perigee point is close; the maneuver is applied at the perimeno point to ensure that the satellite's aphelion height is the same; the reference star is determined, and the rest The satellite is a tracking star, and the phase angle of the tracking star is guaranteed to be the same as that of the reference star by using two near-moon point adjustment movements; finally, the optimal two-pulse or multi-pulse rendezvous is used to make the speed and position of...
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