Cart (Loading....) | Create Account
Close category search window
 

Control topologies for deep space formation flying spacecraft

Sign In

Cookies must be enabled to login.After enabling cookies , please use refresh or reload or ctrl+f5 on the browser for the login options.

The purchase and pricing options are temporarily unavailable. Please try again later.
2 Author(s)
Smith, R.S. ; Dept. of Electr. & Comput. Eng., California Univ., Santa Barbara, CA, USA ; Hadaegh, F.Y.

A deep space satellite formation can be specified in terms of the relative satellite positions and absolute satellite orientations. Redundancy in the relative position specification generates a family of control topologies with equivalent stability and reference tracking performance. We give a characterization of this equivalence and show that there exists a control topology which achieves a global tracking objective using only local controllers. This local relative topology can be implemented without requiring communication between the formation spacecraft.

Published in:

American Control Conference, 2002. Proceedings of the 2002  (Volume:4 )

Date of Conference:

2002

Need Help?


IEEE Advancing Technology for Humanity About IEEE Xplore | Contact | Help | Terms of Use | Nondiscrimination Policy | Site Map | Privacy & Opting Out of Cookies

A not-for-profit organization, IEEE is the world's largest professional association for the advancement of technology.
© Copyright 2014 IEEE - All rights reserved. Use of this web site signifies your agreement to the terms and conditions.