Design and Implementation of a Hardware-in-the-Loop Simulation System for a Tilt Trirotor UAV
Journal of Advanced Transportation, 2020 The tilt trirotor unmanned aerial vehicle (UAV) is a novel aircraft that has broad application prospects in transportation. However, the development progress of the aircraft is slow due to the complicated control system and the high cost of the flight ...
Li Yu +4 more
doaj +12 more sources
Attitude and Altitude Control of Trirotor UAV by Using Adaptive Hybrid Controller [PDF]
Journal of Control Science and Engineering, 2016 The paper presents an adaptive hybrid scheme which is based on fuzzy regulation, pole-placement, and tracking (RST) control algorithm for controlling the attitude and altitude of trirotor UAV.
Zain Anwar Ali +3 more
doaj +6 more sources
Hovering of coaxial Trirotor helicopter constructed with coaxial mechanism driven by a motor
Transactions of the JSME (in Japanese), 2014 This paper proposes a coaxial trirotor helicopter constructed with coaxial mechanism driven by one motor. There two types of trirotor unmanned aerial vehicles (UAVs) are existed.
Yoshihiro Takita
exaly +5 more sources
D37 Hovering of coaxial Trirotor helicopter constructed with coaxial mechanism driven by a motor
The Proceedings of the Symposium on the Motion and Vibration Control, 2013 Yoshihiro Takita
exaly +4 more sources
Gong-H: Design, Analysis and Control of a Tilt Trirotor Aircraft with Tandem Wings
DronesVertical take-off and landing (VTOL) configurations incur a structural weight penalty that reduces payload fraction and endurance compared to conventional fixed-wing and multirotor aircraft of comparable gross weight. To extend the endurance of VTOL UAVs,
Zemin Lin +3 more
doaj +2 more sources
Attitude control method for tilt-trirotor UAV based on adaptive fuzzy PID
Journal of Physics: Conference SeriesAbstract This study introduces an adaptive fuzzy PID control-based approach for managing the attitude of a tilt-trirotor unmanned aerial vehicle (UAV). This approach employs fuzzy logic to dynamically adjust the parameters of the PID controller in real time, enabling the control system to effectively adapt to changing flight conditions ...
Yukang Jin +3 more
exaly +2 more sources
Nonlinear Control of a Single Tail Tilt Servomotor Tri-Rotor Ducted VTOL-UAV
Aerospace, 2022 This paper explores a novel single tail tilt servomotor tri-rotor ducted vertical takeoff and landing unmanned aerial vehicle system (VTOL-UAV), and proposes a compound control method combining disturbance observer, model predictive control (MPC) and ...
Yanpeng Hu +4 more
doaj +1 more source
Performance evaluation of RW‐Quadrotor and Bi‐Quadrotor for payload delivery
IET Intelligent Transport Systems, Volume 17, Issue 11, Page 2221-2236, November 2023., 2023 In this paper, we propose an adaptive backstepping controller for both RW‐Quadrotor and Bi‐Quadrotor to handle mass change during the same mission and evaluation of the performance of both UAVs under four aspects: (i) trajectory tracking, (ii) speed, (iii) mission timing and (iv) Energy consumption.
Nihal Dalwadi +2 more
wiley +1 more source
Conversion control of a tilt tri-rotor unmanned aerial vehicle with modeling uncertainty
International Journal of Advanced Robotic Systems, 2021 The tilt-rotor unmanned aerial vehicle (TRUAV) has vertical take-off and landing and high-speed flight capabilities through conversion and reconversion modes, thereby presenting wide application prospects.
Chao Chen +4 more
doaj +1 more source
Actuators, 2023 In this paper, a new nonlinear robust fault-tolerant tracking control method is proposed for a tri-rotor unmanned aerial vehicle (UAV) under unknown abnormal actuator behaviors together with unknown external disturbances.
Wenlai Ma +4 more
doaj +1 more source