A control method for spacecraft rendezvous between orbits of unstable translation points of the sun-earth system
A control method and track rendezvous technology, applied in the direction of non-electric variable control, adaptive control, general control system, etc., can solve the problems of model error influence, open-loop control susceptible to external interference, etc., to overcome navigation error and meet real-time Sexual needs, effects of overcoming limitations in normal rendezvous
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[0041]In order to make the technical problems solved by the present invention, the technical solutions adopted and the technical effects achieved clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, but not to limit the present invention. In addition, it should be noted that, for the convenience of description, only parts related to the present invention are shown in the drawings but not all content.
[0042] image 3 The implementation flow chart of the control method for spacecraft rendezvous between orbits of unstable translation points of the sun-earth system provided by the embodiment of the present invention. Such as image 3 As shown, the spacecraft rendezvous control method provided by the embodiment of the present invention between the orbits of the unstable translation...
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