A Space Debris Avoidance Maneuvering Method for Remote Sensing Satellites Based on Trajectory Keeping Requirements
A technology for remote sensing satellites and space debris, applied in the field of spacecraft control, can solve the problems of ambiguity in the adjustment of evasive maneuvers, difficulty in popularization and application, and large randomness, etc., to achieve the goal of improving early warning and evasion capabilities, saving propellant, and low cost Effect
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[0040] Since most remote sensing satellites are earth observation imaging satellites, their mission characteristics determine that satellites have relatively strict requirements on the distribution of ground trajectories. Therefore, when maneuvering to avoid the threat of space debris collisions, the mission characteristics of satellites can be used , combined with the satellite's demand for trajectory keeping, deduce the satellite's quantitative demand for maneuvering, so as to quantitatively formulate a reasonable avoidance strategy.
[0041] The following concepts are used in the maneuvering method for avoiding space debris of remote sensing satellites based on track keeping requirements in the present invention:
[0042] Return orbit: The orbit in which the ground track of the satellite repeats at its original position after an integer number of days. This integer number of days is called the return cycle.
[0043] Track keeping: For low-orbit remote sensing satellites, wh...
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