Cooperative Orbit Determination Method Based on Optical Observation of Space Objects by Constellation
A space target and optical technology, applied in the field of aerospace, can solve problems such as inability to determine orbit, insufficient orbit determination accuracy, and low orbit determination efficiency, and achieve the effects of improving orbit determination accuracy, improving overall performance, and accelerating convergence speed
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[0025] In order to better illustrate the purpose and advantages of the present invention, the content of the invention will be further described below in conjunction with the accompanying drawings and examples.
[0026] Such as figure 1 As shown, the coordinated orbit determination method based on the optical observation of space targets disclosed by this embodiment, the specific implementation steps are as follows:
[0027] Step 1: Based on the two-body dynamic model of the spacecraft relative to the central celestial body, construct the state model of the constellation optical observation collaborative orbit determination system.
[0028] When the spacecraft is in orbit, considering the two-body model of the spacecraft and the central celestial body, the orbital dynamics are shown in Equation (5).
[0029]
[0030] where r i (i=1,2,3,4) is the position vector of the i-th observed star relative to the central celestial body, v i (i=1,2,3,4) is the velocity vector of the...
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