DMOC
Author: Tianjiang Shuo
Website: https://cislunarspace.cn
Definition
A direct local optimal control method based on direct discretization of the variational structure of the mechanical system (Lagrange-d'Alembert principle), using forced discrete Euler-Lagrange equations as equality constraints for nonlinear optimization solved by SQP.
Application Value
This concept has application value in cislunar space research and engineering practice, helping to understand core principles of the field.
Related Concepts
- Monte Carlo Trajectory Shooting, MCTS
- Powered Lunar Flyby, PLF
- Planar Circular Restricted Three-Body Problem, PCRTBP
- Insertion Delta-V
References
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