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Deployment control system for spacecraft having to fly in formation using simultaneous high precision determination of their positions
Deployment control system for spacecraft having to fly in formation using simultaneous high precision determination of their positions
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机译:用于航天器的部署控制系统,必须同时高精度确定其位置才能飞入编队
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摘要
The system has a calculation module (MC1) determining operations, intended to position each of reference and follower space vehicles (ES1, ES2) at a chosen instant in a chosen position with respect to a reference path (TR), based on orbital positions of the vehicles by considering a time law of the reference vehicle for placing a formation in a chosen configuration. Calculation units (MC21, MC22) communicate anti-collision operations, determined when a risk of collision of one vehicle with the other vehicle exceeds a chosen value, with orbit correction modules (MCO1, MCO2).
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