Satellite team configuring control method based on fuel consumption optimization
A technology of satellite formation and control method, which is applied in the field of configuration control of satellite formation, and can solve problems such as complex fuel consumption and non-optimum
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[0030] The present invention will be described in detail below in conjunction with specific embodiments. The following examples will help those skilled in the art to further understand the present invention, but do not limit the present invention in any form. It should be noted that those skilled in the art can make several modifications and improvements without departing from the concept of the present invention. These all belong to the protection scope of the present invention.
[0031] Such as figure 1 As shown, record the master star as C and the slave star as A. With the main star C as the center, the formation coordinate system Cxyz is established. The x-axis deviates from the center of the earth along the radial direction in the orbital plane of the main star, the z-axis is the normal of the orbital plane of the main star, and the y-axis is determined by the right-hand rule, and the direction is consistent with the speed direction of the main star satellite.
[0032...
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