Energy control method for high-precision orbit control of inclined-orbit marine dynamic satellites
A technology of inclined orbit and energy control, applied in the direction of motor vehicles, space navigation equipment, space navigation aircraft, etc., to ensure the energy safety of the whole star
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[0057] In order to make the objectives, technical solutions and advantages of the present invention clearer, the embodiments disclosed in the present invention will be described in further detail below with reference to the accompanying drawings.
[0058] like figure 1 In order to make the marine dynamic environment satellite have high-precision and high-resolution marine geoid measurement data, high requirements are placed on the accuracy of satellite orbit maintenance. Generally, the maximum drift range of the ground trajectory is required to be better than 1km, and the satellite control system requires the realization of The following requirements:
[0059] The track semi-major axis error is less than 1m;
[0060] The orbit inclination error is less than 0.007°;
[0061] The eccentricity is not more than 0.00007;
[0062] The error of the argument of perigee is less than 3.5°.
[0063] Taking the example of the non-sun-synchronous return frozen orbit of 66°, the...
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