Improved sequential convex programming using modified Chebyshev–Picard iteration for ascent trajectory optimization

This paper presents an improved sequential convex programming (SCP) algorithm for ascent trajectory optimization of launch vehicles, by exploiting the state-of-the-art modified Chebyshev–Picard iteration (MCPI) technique. In the proposed algorithm, the MCPI technique is first utilized to transcribe...

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Bibliographic Details

Published in:	Aerospace science and technology Vol. 120; p. 107234
Main Authors:	Ma, Yangyang, Pan, Binfeng, Hao, Chuanchuan, Tang, Shuo
Format:	Journal Article
Language:	English
Published:	Elsevier Masson SAS 01.01.2022
Subjects:	Launch vehicle Modified Chebyshev–Picard iteration Sequential convex programming Trajectory optimization Launch vehicle Sequential convex programming Modified Chebyshev–Picard iteration Trajectory optimization
ISSN:	1270-9638, 1626-3219
Online Access:	Get full text
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