An Integrated Altitude Control Design for a Tail-Sitter UAV Equipped With Turbine Engines

An Integrated Altitude Control Design for a Tail-Sitter UAV Equipped With Turbine Engines

An accurate and robust altitude controller is critical for vertical takeoff and landing (VTOL) unmanned aerial vehicles (UAVs) in achieving quasi-stationary flight. Most UAV altitude control designs neglect the rotor dynamics. Therefore, they cannot be used for a tail-sitter UAV equipped with turbin...

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Bibliographic Details
Main Authors: Huanyu Li, Chunwen Li, Hangyu Li, Yingjie Li, Zhipeng Xing
Format: Article
Language:English
Published: IEEE 2017-01-01
Series:IEEE Access
Subjects:
Tail-sitter UAV
turbine engine
time delay
altitude control
acceleration feedback
Online Access:https://ieeexplore.ieee.org/document/7933945/

Internet

https://ieeexplore.ieee.org/document/7933945/

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