c-planelles/self-propelled-satellites
The system is formed by self-propelled satellites influenced by the Sun whose objective is not to leave the domain maintaining the maximum possible speed.
This project simulates the movement of self-propelled satellites influenced by celestial bodies like the Sun, aiming to keep them within a defined area while maximizing their speed. It takes initial conditions for satellites and celestial body positions, and outputs the optimized satellite trajectories and propulsion strategies. This would be useful for space mission designers or astrodynamicists exploring autonomous navigation and station-keeping.
No commits in the last 6 months.
Use this if you need to model autonomous spacecraft behavior in gravitational fields to maintain position and achieve maximum velocity.
Not ideal if you are looking for a high-fidelity orbital mechanics simulator for precise mission planning, as this focuses on evolutionary optimization.
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Processing
License
MIT
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Last pushed
Nov 14, 2017
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