Quaternion-Based Attitude Control System Design of Single and Cooperative Spacecrafts: Boundedness of Solution Approach

Quaternion-Based Attitude Control System Design of Single and Cooperative Spacecrafts: Boundedness of Solution Approach

It is well known that single equilibrium orientation point in matrix rotation is represented by two equilibrium points in quaternion. This fact would imply nonefficient control effort as well as problem in guaranteeing stability of the two equilibrium points in quaternion. This paper presents a solu...

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Bibliographic Details
Main Authors:	Harry Septanto, Riyanto T. Bambang, Arief Syaichu-Rohman, Ridanto Eko Poetro, Adrianto Ravi Ibrahim
Format:	Article
Language:	English
Published:	Hindawi Limited 2014-01-01
Series:	Modelling and Simulation in Engineering
Online Access:	http://dx.doi.org/10.1155/2014/652571

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