Optimal Guidance for Heliocentric Orbit Cranking with E-Sail-Propelled Spacecraft
In astrodynamics, orbit cranking is usually referred to as an interplanetary transfer strategy that exploits multiple gravity-assist maneuvers to change both the inclination and eccentricity of the spacecraft osculating orbit without changing the specific mechanical energy, that is, the semimajor ax...
| 發表在: | Aerospace |
|---|---|
| 主要作者: | |
| 格式: | Article |
| 語言: | 英语 |
| 出版: |
MDPI AG
2024-06-01
|
| 主題: | |
| 在線閱讀: | https://www.mdpi.com/2226-4310/11/6/490 |