Prompt Content
Design an optimal control algorithm (e.g., MPC, LQR with path planning) to guide the chaser spacecraft from an initial offset to a safe docking port on the target satellite. Focus on minimizing fuel consumption while respecting thrust magnitude constraints and avoiding keep-out zones. Explain how you'll manage the transition from far-field rendezvous to close-proximity operations. This relates directly to the 'RPO_DockingScenario' evaluation task.
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