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Orbital Mechanics & Optimization Core
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Linked challenge: AI-Driven Space Logistics & Constellation Deployment Optimization with Falcon 180B
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Linked challenge
AI-Driven Space Logistics & Constellation Deployment Optimization with Falcon 180B
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Implement the core orbital mechanics simulation and a multi-objective optimization algorithm to generate feasible OTV trajectories. Your optimizer should take an OTV's initial state and a list of target orbits for multiple payloads, and output a sequence of maneuvers (e.g., Hohmann transfers, plane changes) that minimizes fuel consumption while adhering to deployment windows and total mission duration. Explain your chosen optimization approach and how it handles constraints.
Adaptation plan
Keep the source stable, then change the prompt in a predictable order so the next run is easier to evaluate.
Keep stable
Hold the task contract and output shape stable so generated implementations remain comparable.
Tune next
Update libraries, interfaces, and environment assumptions to match the stack you actually run.
Verify after
Test failure handling, edge cases, and any code paths that depend on hidden context or secrets.