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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| Published in: | Aerospace science and technology Vol. 80; pp. 38 - 55 |
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| Main Authors: | , , , |
| Format: | Journal Article |
| Language: | English |
| Published: |
Elsevier Masson SAS
01.09.2018
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| Subjects: | |
| ISSN: | 1270-9638, 1626-3219 |
| Online Access: | Get full text |
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