Optimization of Geostationary Orbit Transfers via Combined Chemical–Electric Propulsion

For geostationary orbit transfers, a long duration is required using electric propulsion and a large propellant mass is needed with chemical propulsion. Hybrid transfers can achieve a balance between the fuel consumption and transfer time. In this paper, a trajectory optimization method is proposed...

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Principais autores:	Shihai Yang, Bo Xu, Xin Li
格式:	Artigo
語言:	Inglês
出版:	MDPI AG 2022-04-01
叢編:	Aerospace
主題:	orbital transfer combined chemical–electric propulsion indirect method geostationary orbit trajectory optimization
在線閱讀:	https://www.mdpi.com/2226-4310/9/4/200
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