Results 51 to 60 of about 3,121 (160)
In our work, an algorithm is presented for tilt-rotor UAV clusters in an unknown complex environment, which addresses the challenge of navigating and positioning in complex unknown environments without external navigation and positioning information.
Liben Yang +3 more
doaj +1 more source
Pigeon-Inspired Transition Trajectory Optimization for Tilt-Rotor UAVs
The continuous configuration changes and velocity variations of tilt-rotor UAVs during the transition phase pose significant challenges to flight safety. Hence, the transition phase trajectory must be specially designed.
Jinlai Deng +5 more
doaj +1 more source
Thrust Vectoring Control of a Novel Tilt-Rotor UAV Based on Backstepping Sliding Model Method. [PDF]
Yu Z, Zhang J, Wang X.
europepmc +1 more source
A Dynamic RCS and Noise Prediction and Reduction Method of Coaxial Tilt-Rotor Aircraft Based on Phase Modulation. [PDF]
Wang Z, Huang J, Yi M, Lu S.
europepmc +1 more source
Design, Analysis, and Testing of a Hybrid VTOL Tilt-Rotor UAV for Increased Endurance. [PDF]
Panigrahi S, Krishna YSS, Thondiyath A.
europepmc +1 more source
The unmanned quad tilt-rotor eVTOL (QTRV) is a variable-configuration aircraft that combines the features of vertical takeoff and landing (VTOL), hovering, and high-speed cruising, making its control system design particularly challenging.
Bohai Deng +3 more
doaj +1 more source
Most industrial rotors supported in active magnetic bearings (AMBs) are operated well below the first bending critical speed. Also, they are usually controlled using proportional, integral and derivative controllers, which are set up as modally uncoupled
Timothy Dimond +4 more
doaj +1 more source
Dynamic Simulation of Tilted Rotor Quadcopter
Application of quadcopter unmanned aerial vehicle (UAV) has already become common today. As the name suggests, quadcopter has four rotors and these rotors can be classified into two types: fixed and tilted rotors. The maneuvering of quadcopter using the fixed rotor is achieved through the thrust differential.
Muhammad Nur Akmal Noor ‘Adzam +3 more
openaire +1 more source
Establishment and Verification of the UAV Coupled Rotor Airflow Backward Tilt Angle Controller
At present, all the flight controllers of agricultural UAVs cannot accurately and quickly control the influencing factors of the UAV coupled rotor airflow backward tilt angle during the application process.
Han Wu +9 more
doaj +1 more source
This study addresses the challenge of excessive downwash generated by uncrewed aerial vehicles (UAVs) during pinpoint weeding in agriculture. We propose a novel UAV design incorporating adaptive rotors that can tilt during flight to reduce the downward ...
Kenki Miyahara +3 more
doaj +1 more source

