Reconfigurable fault tolerant flight control based on Nonlinear Model Predictive Control-Reference-Cited by-同舟云学术

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Reconfigurable fault tolerant flight control based on Nonlinear Model Predictive Control

Published:2013-06 Issue: Volume: Page:
ISSN:
Container-title:2013 American Control Conference
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Author:

Kufoalor D. K.,Johansen T. A.

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/6573242/6579790/06580635.pdf?arnumber=6580635

Cited by 6 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Hierarchical Adaptive Fault-Tolerant Model Predictive Control of a Quadrotor;New Achievements in Unmanned Systems;2023

2. A Fault-Tolerant Control Scheme for Fixed-Wing UAVs with Flight Envelope Awareness;Journal of Intelligent & Robotic Systems;2021-05-27

3. LMI-based adaptive output feedback fault-tolerant controller design for nonlinear systems;International Journal of Adaptive Control and Signal Processing;2017-08-31

4. Angle of Attack and Load Factor Limiting in Fighter Aircraft using Command Governors;AIAA Guidance, Navigation, and Control Conference;2017-01-05

5. Non-linear Model Predictive Control for Longitudinal and Lateral Guidance of a Small Fixed-Wing UAV in Precision Deep Stall Landing;AIAA Infotech @ Aerospace;2016-01-01

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