Abstract
The orbital game theory is a fundamental technology for the cleanup of space debris to improve the safety of useful spacecraft in future, thus, this work develops a decision-making method by reinforcement learning technology to implement the pursuit-evasion game in elliptical orbits. The linearized Tschauner-Hempel equation describes the spacecraft's motion and the problem is formulated by game theory. Subsequently, an impulsive maneuvering model in a complete three-dimensional elliptical orbit is established. Then an algorithm based on deep deterministic policy gradient is designed to solve the optimal strategy for the pursuit-evasion game. For the successful decision of the pursuer, an extensive reward function is designed and improved considering the shortest time, optimal fuel, and collision avoidance. Finally, numerical simulations of a pursuit-evasion mission are performed to demonstrate the effectiveness and superiority of the proposed decision-making algorithm. The game success rate of the algorithm against targets with different maneuvering abilities is verified, which implies that the algorithm can be applied in extended scenarios.
| Original language | English |
|---|---|
| Article number | 106072 |
| Journal | Control Engineering Practice |
| Volume | 153 |
| DOIs | |
| State | Published - Dec 2024 |
Keywords
- Decision making
- Deep deterministic policy gradient
- Elliptical orbit
- Impulsive maneuver
- Pursuit-evasion game
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