Fault-Tolerant Reduced-Attitude Control for Spacecraft Constrained Boresight Reorientation
Author:
Affiliation:
1. Beihang University, 100191 Beijing, People’s Republic of China
2. York University, Toronto, Ontario M3 J 1P3, Canada
3. Concordia University, Montreal, Quebec H3G 1M8, Canada
Funder
National Natural Science Foundation of China
Beijing Natural Science Foundation
China Postdoctoral Science Foundation
National Key Basic Research Program–“Gravitational Wave Detection”Project
Stable Supporting Fund of the Science and Technology on Space Intelligent Control Laboratory
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/pdf/10.2514/1.G006651
Reference40 articles.
1. Reduced-Attitude Boresight Guidance and Control on Spacecraft for Pointing, Tracking, and Searching
2. The attitude control problem
3. Adaptive Control of Nonlinear Attitude Motions Realizing Linear Closed Loop Dynamics
4. New Results for Time-Optimal Three-Axis Reorientation of a Rigid Spacecraft
5. Robust Saturated Finite-Time Attitude Control for Spacecraft Using Integral Sliding Mode
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