Optimal large-angle attitude control of rigid spacecraft by momentum transfer-Reference-Cited by-同舟云学术

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Optimal large-angle attitude control of rigid spacecraft by momentum transfer

Published:2007-05-01 Issue:3 Volume:1 Page:657-664
ISSN:1751-8644
Container-title:IET Control Theory & Applications
language:en
Short-container-title:

Author:

Yang C.-C.,Wu C.-J.

Publisher

Institution of Engineering and Technology (IET)

Subject

Electrical and Electronic Engineering,Control and Optimization,Computer Science Applications,Human-Computer Interaction,Control and Systems Engineering

Link

https://digital-library.theiet.org/content/journals/10.1049/iet-cta_20060132?crawler=true&mimetype=application/pdf

Reference23 articles.

1. Minimum fuel spacecraft reorientation

2. Optimal Continuous Torque Attitude Maneuvers

3. New results on the optimal spacecraft attitude maneuver problem

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