Fault-Tolerant Guidance of Rocket Vertical Landing Phase Based on MPC Framework

For the vertical landing process of reusable rockets, the landing accuracy is likely to be affected by disturbances and faults during flight. In this paper, a fault-tolerant guidance method based on the MPC framework is put forward. First, we propose a piecewise guidance algorithm that combines a tr...

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Vydáno v:	International Journal of Aerospace Engineering Ročník 2022; s. 1 - 11
Hlavní autoři:	Li, Jingqi, Long, Yaosong, Su, Mao, Liu, Lei, Wang, Bo, Cheng, Zhongtao
Médium:	Journal Article
Jazyk:	angličtina
Vydáno:	New York Hindawi 12.08.2022 John Wiley & Sons, Inc Wiley
Témata:	Accuracy Aerospace engineering Algorithms Atmospheric density Closed loops Computational geometry Control systems Convex analysis Convexity Design Deviation Disturbances Drag coefficients Electronics in navigation Experiments Fault tolerance Mathematical optimization Methods Navigation systems Optimization algorithms Reusable rocket engines Robustness Rockets Spacecraft guidance System failures Trajectory optimization Velocity Vertical landing
ISSN:	1687-5966, 1687-5974
On-line přístup:	Získat plný text
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