Dual Quaternion Based Close Proximity Operation for In-Orbit Assembly via Model Predictive Control

This paper studies the problem of guidance and control for autonomous in-orbit assembly. A six-degree-of-freedom (6-DOF) motion control for in-orbit assembly close proximity operation between a service satellite and a target satellite is addressed in detail. The dynamics based on dual quaternion are...

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Bibliographic Details
Main Authors: Chuqi Sun, Yan Xiao, Zhaowei Sun, Dong Ye
Format: Article
Language:English
Published: Wiley 2021-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2021/1305095
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