Optimal Path Planning-Based Finite-Time Control for Agile CubeSat Attitude Maneuver

Optimal Path Planning-Based Finite-Time Control for Agile CubeSat Attitude Maneuver

A finite-time controller based on optimal path planning was developed for the agile CubeSat attitude maneuver. This achieved a stable attitude large-angle maneuver just by using momentum wheels and a magnetorquer, which is unlike other larger satellites that need a control moment gyroscope or thrust...

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Bibliographic Details
Main Authors: Xiaohua Zhang, Xiang Zhang, Zhengliang Lu, Wenhe Liao
Format: Article
Language:English
Published: IEEE 2019-01-01
Series:IEEE Access
Subjects:
CubeSat
attitude maneuver
path planning
quintic polynomial
differential evolution
finite-time control
Online Access:https://ieeexplore.ieee.org/document/8756274/

Internet

https://ieeexplore.ieee.org/document/8756274/

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