Rigid-Body Pose Hybrid Control Using Dual Quaternions: Global Asymptotic Stabilization and Robustness
Author:
Affiliation:
1. University of Arizona, Tucson, Arizona 85721
2. University of California, Santa Cruz, Santa Cruz, California 95064
Funder
CITRIS and the Banatao Institute at the University of California
Air Force Office of Scientific Research
Air Force Research Laboratory
AFOSR Center of Excellence Award
NSF
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.G004621
Reference33 articles.
1. Inertia-Free Spacecraft Attitude Tracking with Disturbance Rejection and Almost Global Stabilization
2. Robust attitude stabilization of spacecraft using nonlinear quaternion feedback
3. Global set stabilization of the spacecraft attitude control problem based on quaternion
4. Satellite Attitude Control by Quaternion-Based Backstepping
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