A geodesic feedback law to decouple the full and reduced attitude
Author:
Publisher
Elsevier BV
Subject
Electrical and Electronic Engineering,Mechanical Engineering,General Computer Science,Control and Systems Engineering
Reference34 articles.
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4. A. Sanyal, A. Fosbury, N.A. Chaturvedi, D.S. Bernstein, Inertia-free spacecraft attitude trajectory tracking with internal-model-based disturbance rejection and almost global stabilization, in: Proceedings of the 27th IEEE American Control Conference, 2009, pp. 4830–4835
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