Event-Triggered Sliding Mode Control for Spacecraft Reorientation With Multiple Attitude Constraints
Author:
Affiliation:
1. School of Aeronautics and Astronautics, Sichuan University, Chengdu, China
2. Mechanical Engineering and Automation, Harbin Institute of Technology Shenzhen, Shenzhen, China
Funder
National Natural Science Foundation of China
Research on Innovation and Application of Space Science and Technology
Shenzhen Science and Technology Program
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Subject
Electrical and Electronic Engineering,Aerospace Engineering
Link
http://xplorestaging.ieee.org/ielx7/7/7778228/10109162.pdf?arnumber=10109162
Reference34 articles.
1. Adaptive fault-tolerant control for attitude reorientation under complex attitude constraints
2. Potential Field-Based Sliding Surface Design and Its Application in Spacecraft Constrained Reorientation
3. Robust Fixed-Time Stability: Application to Sliding-Mode Control
4. Event-Triggered Real-Time Scheduling of Stabilizing Control Tasks
5. Dynamic Event-triggered Control and Estimation: A Survey
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