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...
| Published in: | Aerospace |
|---|---|
| Main Author: | Alessandro A. Quarta |
| Format: | Article |
| Language: | English |
| Published: |
MDPI AG
2024-06-01
|
| Subjects: | |
| Online Access: | https://www.mdpi.com/2226-4310/11/6/490 |
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