Autonomous entry guidance using Linear Pseudospectral Model Predictive Control

This paper aims at developing an autonomous entry guidance method that requires no mission-dependent adjustments and will be applicable to a wide range of entry scenarios with worldwide destinations. Firstly, a nonlinear reduced-order entry dynamical system with coupled lateral and longitudinal moti...

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Bibliographic Details
Published in:Aerospace science and technology Vol. 80; pp. 38 - 55
Main Authors: Yang, Liang, Liu, Xiaoming, Chen, Wanchun, Zhou, Hao
Format: Journal Article
Language:English
Published: Elsevier Masson SAS 01.09.2018
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ISSN:1270-9638, 1626-3219
Online Access:Get full text
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