A method and system for unloading angular momentum during orbit change of an all-electric propulsion satellite
A technology of angular momentum unloading and electric propulsion, which is applied in the direction of motor vehicles, space navigation equipment, space navigation equipment, etc., to avoid the effect of attitude loss control
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[0045] Exemplary embodiments of the present disclosure will be described in more detail below with reference to the accompanying drawings. Although exemplary embodiments of the present disclosure are shown in the drawings, it should be understood that the present disclosure may be embodied in various forms and should not be limited by the embodiments set forth herein. Rather, these embodiments are provided for more thorough understanding of the present disclosure and to fully convey the scope of the present disclosure to those skilled in the art. It should be noted that, in the case of no conflict, the embodiments of the present invention and the features in the embodiments can be combined with each other. The present invention will be described in detail below with reference to the accompanying drawings and examples.
[0046] During the orbit change process of the all-electric propulsion satellite, two electric thrusters are used to ignite the orbit change, and two unloading...
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