Velocity Observer-Based Event-Triggered Adaptive Fuzzy Attitude Takeover Control of Spacecraft With Quantized Quaternion
Author:
Affiliation:
1. Research Center of Satellite Technology, Harbin Institute of Technology, Harbin, China
2. Nanyang Technological University, Singapore
Funder
National Natural Science Foundation of China
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Subject
Electrical and Electronic Engineering,Aerospace Engineering
Link
http://xplorestaging.ieee.org/ielx7/7/10213347/10018204.pdf?arnumber=10018204
Reference38 articles.
1. T–S Fuzzy-Based Event-Triggering Attitude-Tracking Control for Elastic Spacecraft With Quantization
2. Decentralized Dynamic Event-Triggered Adaptive Fuzzy Control for Switched Nonlinear Systems With Unstable Inverse Dynamics
3. Fuzzy-Logic-Based Robust Attitude Control of Networked Spacecraft via Event-Triggered Mechanism
4. Fuzzy-based dynamic event triggering formation control for nonstrict-feedback nonlinear MASs
5. Robust Attitude Tracking Control for Spacecraft with Quantized Torques
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