TiltDrone: A fully-actuated tilting quadrotor platform

P Zheng, X Tan, BB Kocer, E Yang… - IEEE Robotics and …, 2020 - ieeexplore.ieee.org
Multi-directional aerial platforms can fly in almost any orientation and direction, often
maneuvering in ways their underactuated counterparts cannot match. A subset of multi …

Bio-inspired classification and evolution of multirotor Micro Aerial Vehicles (MAVs): A comprehensive review

SW Hameed, N Imanberdiyev, E Camci, YW Yun… - Robotics and …, 2024 - Elsevier
Abstract Multirotor Micro Aerial Vehicles (MAVs) have become essential in many
applications like surveillance, disaster management, and aerial inspection. The diverse …

Modeling and experimental study on orientation dynamics of a Mars rotorcraft with swashplate mechanism

K Zhu, D Tang, Q Quan, Y Lv, W Shen… - Aerospace Science and …, 2023 - Elsevier
The Mars rotorcraft is an auxiliary aerial exploration platform to expand the rovers' patrol
range. Attitude control is a fundamental aspect of autonomous flight control. So far, there has …

Gemini ii: Design, modeling, and control of a compact yet efficient servoless bi-copter

Y Qin, N Chen, Y Cai, W Xu… - IEEE/ASME Transactions …, 2022 - ieeexplore.ieee.org
Unmanned aerial vehicles (UAV) are widely used in the field for tasks that require 3-D
movements in space. The simultaneous demand for heavy payload capacity, long operating …

Modelling, control and simulation of a single rotor UAV with swashplateless torque modulation

E Bernardes, F Boyer, S Viollet - Aerospace Science and Technology, 2023 - Elsevier
Single rotor-base unmanned aerial vehicles (UAVs) represent the most minimalistic design
to implement an aerial vehicle. We describe here a mono-rotor UAV, also named mono …

[HTML][HTML] Characterization of different hinge angles for swashplateless micro aerial robots

AT Karasahin - Engineering Science and Technology, an International …, 2024 - Elsevier
Abstract Micro Aerial Robots (MARs) are expected to increase their payload carrying
capacity and flight time, and to serve in limited areas. These demands can only be met by …

Emulating a fully actuated aerial vehicle using two actuators

J Paulos, B Caraher, M Yim - 2018 IEEE International …, 2018 - ieeexplore.ieee.org
Micro air vehicles exemplified by quadrotors generate downward thrust in their body fixed
frame and may only maneuver spatially by changing their orientation. As a result of this …

A directly coil-actuated cyclic pitch control based rotor: Design, modeling, and analysis

Q Wu, D Tang, Q Quan, K Zhu, Y Wu, Z Deng - Aerospace Science and …, 2023 - Elsevier
This work introduces a directly coil-actuated cyclic pitch control method for the swashplate-
less aircraft. This method drives the rotor to rotate periodically around the pitch axis through …

HALO: A Safe, Coaxial, and Dual-Ducted UAV Without Servo

H Li, N Chen, F Kong, Y Zou, S Zhou… - 2023 IEEE/RSJ …, 2023 - ieeexplore.ieee.org
This paper presents a novel uncrewed aerial vehicle (UAV) design named HALO, which
stands for “harmless aerial limber robot”. HALO uses a swashplateless mechanism to …

基于双向电机驱动的四旋翼机动飞行控制

徐力昊, 张宇, 许斌 - 北京航空航天大学学报, 2021 - bhxb.buaa.edu.cn
四旋翼飞行器(QUAV) 的位置, 姿态运动控制效果决定了其机动性. 为了克服四旋翼系统欠驱动
的缺陷, 基于四元数表达对一种双向电机驱动的四旋翼进行了动力学建模 …