Aircraft Attitude Control on High-order Fully Actuated System Theory
Author:
Affiliation:
1. Science and Technology on Complex System Control and Intelligent Agent Cooperation Laboratory
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10243163/10243123/10243292.pdf?arnumber=10243292
Reference6 articles.
1. Low-Power Fault-Tolerant Control for Nonideal High-Order Fully Actuated Systems
2. Substability and Substabilization: Control of Subfully Actuated Systems
3. High-order fully actuated system approaches: Part VIII. Optimal control with application in spacecraft attitude stabilisation
4. Three-axis coupled flight control law design for flying wing aircraft using eigenstructure assignment method
5. High-order system approaches: I. Fully-actuated systems and parametric designs;duan;ACTA Automatica Sinica,2020
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