Autonomous collision avoiding method capable of achieving optimal spacecraft energy under multiple constraints
A collision avoidance, energy-optimized technology for aerospace applications
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[0179] The two-body recursive model is used to give the satellite flight trajectory, and the minimum safe distance is set to 300m. When it is less than 300m, an early warning is issued and collision avoidance control is performed. The effectiveness of the designed optimal control avoidance algorithm is verified by two satellite orbital collision simulations. and feasibility.
[0180] Orbit type constraints: Sun-synchronous orbit is required. After the avoidance control is completed, the orbit is still a sun-synchronous orbit or a near-sun-synchronous orbit. If it is a two-body model orbit, there is no requirement;
[0181] Payload constraints: The payload resolution is 1m (@500km), and the upper limit of the allowable resolution is 1.002m, so the allowable orbital height adjustment is not higher than 501km;
[0182] Control strategy constraints: when the avoiding satellite enters the safe range of the target satellite, avoid the orbit of the target satellite with the optimal a...
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