Nonlinear Proportional-Derivative Control Incorporating Closed-Loop Control Allocation for Spacecraft
Author:
Affiliation:
1. Department of Control Science and Engineering, Harbin Institute of Technology, Heilongjiang 150001, People’s Republic of China
2. Department of Mechanical and Industrial Engineering, Concordia University, Montreal, Quebec H3G 1M8, Canada
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
http://arc.aiaa.org/doi/pdf/10.2514/1.61815
Reference29 articles.
1. Inverse optimal stabilization of a rigid spacecraft
2. Nonlinear Attitude State Tracking Control for Spacecraft
3. Feedback control logic for spacecraft eigenaxis rotations under slew rate and control constraints
4. Nonlinear Adaptive Control of Spacecraft Maneuvers
5. Robust attitude stabilization of spacecraft using nonlinear quaternion feedback
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