Minimum-Time Continuous-Thrust Orbit Transfer
Author: Tianjiang Shuo
Website: https://cislunarspace.cn
Definition
Orbital transfer problem that minimizes time for a spacecraft with steerable continuous thrust of constant magnitude, typically solved using Euler-Lagrange theory and shooting methods.
Application Value
This concept is applicable in cislunar space mission design, orbit optimization, and trajectory planning for spacecraft transfers and maneuver strategies.
Related Concepts
References
- Thorne 1996