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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Vydáno v:	Aerospace science and technology Ročník 117; s. 106965
Hlavní autoři:	Cheng, Guanghui, Jing, Wuxing, Gao, Changsheng
Médium:	Journal Article
Jazyk:	angličtina
Vydáno:	Elsevier Masson SAS 01.10.2021
Témata:	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
On-line přístup:	Získat plný text
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