Design and Evaluation of Fault-Tolerant Electro-Mechanical Actuators for Flight Controls of Unmanned Aerial Vehicles

Design and Evaluation of Fault-Tolerant Electro-Mechanical Actuators for Flight Controls of Unmanned Aerial Vehicles

Electro-mechanical actuators (EMAs) are a primary actuation technology for unmanned aerial vehicles (UAVs). Intensive research has been conducted for designing and evaluating fault-tolerant EMAs for flight controls of UAVs to ensure their compliance with new airworthiness requirements for safe opera...

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Bibliographic Details
Main Authors: Mohamed A. A. Ismail, Simon Wiedemann, Colin Bosch, Christoph Stuckmann
Format: Article
Language:English
Published: MDPI AG 2021-07-01
Series:Actuators
Subjects:
fault-tolerant electro-mechanical actuator
certified UAVs
model-based fault detection
sensorless load monitoring
Online Access:https://www.mdpi.com/2076-0825/10/8/175

Internet

https://www.mdpi.com/2076-0825/10/8/175

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