Research on FCS Design Technology of Electric Tilting Quadrotor UAV

Tilting quadrotor aircraft not only has the advantages of tilting twin-rotor aircraft, such as vertical takeoff and landing, free hovering and long-range transportation, and high-speed cruise, but also can improve the flight performance, carrying capacity and maneuverability of the aircraft. Taking...

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Bibliographic Details
Published in2023 IEEE 23rd International Conference on Software Quality, Reliability, and Security Companion (QRS-C) pp. 654 - 661
Main Authors Xie, Xiaoming, Xu, Jinfa, Shen, Suiyuan, Cao, Wei, Zhang, Guigang
Format Conference Proceeding
LanguageEnglish
Published IEEE 22.10.2023
Subjects
Aerospace control
Aircraft
Autonomous aerial vehicles
control law
Digital simulation
flight control system
Hardware
Quadrotors
simulation model
tilting quadrotor
transition mode
Transportation
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Summary:Tilting quadrotor aircraft not only has the advantages of tilting twin-rotor aircraft, such as vertical takeoff and landing, free hovering and long-range transportation, and high-speed cruise, but also can improve the flight performance, carrying capacity and maneuverability of the aircraft. Taking a 100kg electric tilting quadrotor UAV as the target platform, the design technology of flight control system of the UAV was studied, including the reasonable and feasible system configuration, software and hardware development technology, system control law design technology, and the establishment technology of simulation platform of the system. The results show that the technical approach for the design of the flight control system of the electric tilting quadrotor is effective and can satisfy the operation requirements of the UAV.
ISSN:2693-9371
DOI:10.1109/QRS-C60940.2023.00081