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NASA NTRS · 19920029677

The attitude control problem

Abstract

A general framework for the analysis of the attitude tracking control problem for a rigid body is presented. A large family of globally stable control laws is obtained by using the globally nonsingular unit quaternion representation in a Lyapunov function candidate whose form is motivated by the consideration of the total energy of the rigid body. The controllers share the common structure of a proportional-derivative feedback plus some feedforward which can be zero (the model-independent case), the Coriolis torque compensation, or an adaptive compensation. These controller structures are compared in terms of the requirement on the a priori model information, guaranteed transient performance, and robustness. The global stability of the Luh-Walker-Paul robot end-effector controller is also analyzed in this framework.

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BibTeXRIS

Wen, John Ting-Yung, Kreutz-Delgado, Kenneth. 1991-10-01. The attitude control problem. https://ntrs.nasa.gov/citations/19920029677

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