학술논문

Homogeneous Finite-Time Pose Tracking of Leader–Following Spacecraft Formation Using a Twistor-Based Model.
Document Type
Article
Source
Electronics (2079-9292); Nov2023, Vol. 12 Issue 21, p4451, 12p
Subject
TWISTOR theory
DYNAMICAL systems
SPACE vehicles
ARTIFICIAL satellite attitude control systems
Language
ISSN
20799292
Abstract
Copyright of Electronics (2079-9292) is the property of MDPI and its content may not be copied or emailed to multiple sites or posted to a listserv without the copyright holder's express written permission. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract. (Copyright applies to all Abstracts.)