Fixed-time regulation of spacecraft orbit and attitude coordination with optimal actuation allocation using dual quaternion

Fixed-time regulation of spacecraft orbit and attitude coordination with optimal actuation allocation using dual quaternion

On-orbit service spacecraft with redundant actuators need to overcome orbital and attitude coupling when performing proximity maneuvers. In addition, transient/steady-state performance is required to fulfill the user-defined requirements. To these ends, this paper introduces a fixed-time tracking re...

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Bibliographic Details
Main Authors: Lichao Sun, Yanpei Huang, Haolin Fei, Bo Xiao, Eric M. Yeatman, Allahyar Montazeri, Ziwei Wang
Format: Article
Language:English
Published: Frontiers Media S.A. 2023-02-01
Series:Frontiers in Robotics and AI
Subjects:
dual quaternion
spacecraft control
fixed-time stability
control torque allocation
optimization
Online Access:https://www.frontiersin.org/articles/10.3389/frobt.2023.1138115/full

Internet

https://www.frontiersin.org/articles/10.3389/frobt.2023.1138115/full

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