Low-Thrust Optimization
Author: Tianjiang Shuo Website: https://cislunarspace.cn
Definition
Numerical methods for optimizing low-thrust trajectories, including indirect and direct methods.
Application Value
This control method can be applied to spacecraft attitude stabilization, orbit keeping, and maneuver trajectory optimization in cislunar space missions, improving mission execution flexibility and reliability.
References
- Ross 等 - 2022 - Dynamical systems, the three-body problem, and space mission design