Constrained Attitude Control for Flexible Spacecraft: Attitude Pointing Accuracy and Pointing Stability Improvement
Author:
Affiliation:
1. Electrical Engineering Department, Iran University of Science and Technology, Tehran, Iran
2. Future Technology Research Center, National Yunlin University of Science and Technology, Douliu, Taiwan
Funder
National Science and Technology Council (NSTC), Taiwan
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Subject
Electrical and Electronic Engineering,Computer Science Applications,Human-Computer Interaction,Control and Systems Engineering,Software
Link
http://xplorestaging.ieee.org/ielx7/6221021/10045573/09874914.pdf?arnumber=9874914
Reference30 articles.
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4. PI-Funnel Control for Two Mass Systems
5. Barrier Function-Based Nonsingular Finite-Time Tracker for Quadrotor UAVs Subject to Uncertainties and Input Constraints
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