Aircraft Wing Ice Online Detection and Fault-Tolerant Control Law Design-Reference-Cited by-同舟云学术

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Aircraft Wing Ice Online Detection and Fault-Tolerant Control Law Design

Published:2021-10-22 Issue: Volume: Page:
ISSN:
Container-title:2021 China Automation Congress (CAC)
language:
Short-container-title:

Author:

Ding Di¹,Qian Wei Q.²,Wang Qing²

Affiliation:

1. China Aerodynamics Research and Development Centre,State Key Laboratory of Aerodynamics China Aerodynamics Research and Development Centre Computational Aerodynamics Institute,Mianyang,China,621000

2. China Aerodynamics Research and Development Centre,Computational Aerodynamics Institute,Mianyang,China,621000

Funder

National Natural Science Foundation of China

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/9727224/9727236/09728535.pdf?arnumber=9728535

Reference22 articles.

1. Active Fault Tolerant Control of a quadrotor UAV based on gainscheduled PID control

2. Fault-Tolerant Control of Quadrotor Helicopter Using Gain-Scheduled PID and Model Reference Adaptive Control

3. The Fractional Order PID Method with a Fault Tolerant Module for Road Feeling Control of Steer-by-Wire System

4. Adaptive Neural Networks-Based Dynamic Inversion Applied to Reconfigurable Flight Control and Envelope Protection Under Icing Conditions

5. Fault-Tolerant Flight Control for Aircraft Wing Icing Based on Icing Detection Method

Cited by 1 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. UAV Icing: A Survey of Recent Developments in Ice Detection Methods;IFAC-PapersOnLine;2023

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