A Convex Optimization Framework for 6-DOF Lunar Powered Descent with a Normalized Finite Rotation Parameterization
There has been increasing interest in the Moon for deep space exploration missions in the last few decades. To accommodate fuel-optimal lunar landing missions, it is essential to develop a fast trajectory planning algorithm considering constrained six-degree-of-freedom (6-DOF) dynamics. On the one h...
Zapisane w:
| Główni autorzy: | , |
|---|---|
| Format: | Artigo |
| Język: | Inglês |
| Wydane: |
MDPI AG
2026-03-01
|
| Seria: | Aerospace |
| Hasła przedmiotowe: | |
| Dostęp online: | https://www.mdpi.com/2226-4310/13/4/300 |
| Etykiety: |
Nie ma etykietki, Dołącz pierwszą etykiete!
|