Recovery trajectory planning for the reusable launch vehicle

Trajectory planning method for the entire recovery process of the reusable launch vehicle is studied. Firstly, a revised trajectory correction method (RTCM) is proposed to reduce the maximum normal aerodynamic load in the endo-atmosphere unpowered descent phase and improve the vehicle's landing...

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Veröffentlicht in:	Aerospace science and technology Jg. 117; S. 106965
Hauptverfasser:	Cheng, Guanghui, Jing, Wuxing, Gao, Changsheng
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	Elsevier Masson SAS 01.10.2021
Schlagworte:	Compound trajectory planning method Particle swarm optimization algorithm Polynomial guidance law Reusable launch vehicle Trajectory correction Polynomial guidance law Reusable launch vehicle Compound trajectory planning method Trajectory correction Particle swarm optimization algorithm
ISSN:	1270-9638, 1626-3219
Online-Zugang:	Volltext
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