Antisaturation Attitude and Orbit-Coupled Control for Spacecraft Final Safe Approach Based on Fast Nonsingular Terminal Sliding Mode
Author:
Affiliation:
1. Ph.D. Student, School of Astronautics, Harbin Institute of Technology, Harbin, Heilongjiang 150001, China (corresponding author).
2. Professor, School of Astronautics, Harbin Institute of Technology, Harbin, Heilongjiang 150001, China.
Publisher
American Society of Civil Engineers (ASCE)
Subject
Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering
Link
http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000993
Reference27 articles.
1. Model Predictive Control approach for guidance of spacecraft rendezvous and proximity maneuvering
2. Sliding-Mode Control Strategies for Rendezvous and Docking Maneuvers
3. Formation control of multiple Euler-Lagrange systems via null-space-based behavioral control
4. Adaptive tracking control of uncertain MIMO nonlinear systems with input constraints
5. Safety Control for Spacecraft Autonomous Rendezvous and Docking Under Motion Constraints
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