Shape Change Maneuvers for Attitude Control of Underactuated Satellites.

An asymptotically stable set point control law is introduced for attitude control of the underactuated spacecraft of a satellite system through its appendage shape changes. It is proposed that rotational maneuvers of the spacecraft are possible while simultaneously achieving a desired shape if the t...

Bibliographic Details
Main Authors:	Ashrafiuon, Hashem., Erwin, R. Scott.
Format:	Villanova Faculty Authorship
Language:	English
Published:	2005
Online Access:	http://ezproxy.villanova.edu/login?url=https://digital.library.villanova.edu/Item/vudl:173915

Main Authors:

Ashrafiuon, Hashem., Erwin, R. Scott.

Format:

Villanova Faculty Authorship

Language:

English

Published:

2005

Online Access:

http://ezproxy.villanova.edu/login?url=https://digital.library.villanova.edu/Item/vudl:173915

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Shape Change Maneuvers for Attitude Control of Underactuated Satellites.

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