Walker constellation deployment method based on double berthing orbits
A technology for parking orbits and orbits, applied in three-dimensional position/channel control, non-electric variable control, instruments, etc., can solve the problems of heavy satellite mass, long cycle, low cost of launch deployment, etc., and achieve the effect of optimizing the angle of deployment accuracy
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[0034]Below in conjunction with accompanying drawing, preferred embodiment of the present invention is described in further detail:
[0035] Such as figure 1 As shown, this example provides a Walker constellation deployment method based on dual berthing orbits, including the following steps:
[0036] Step S1, sending the satellites used to deploy the Walker constellation into the first parking orbit and the second parking orbit respectively;
[0037] Step S2, the first satellite enters the working orbit through orbital maneuvering, and the remaining satellites stay in the first parking orbit and the second parking orbit;
[0038] Step S3, waiting for the orbital plane of the current parking orbit to precess relative to the orbital plane of the working orbit where the adjacent satellite is located until the right ascension of the ascending node differs from the preset angle, the next satellite enters the working orbit through orbital maneuvering; and so on until All satellite...
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