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相关论文: Planning and Control for a Dynamic Morphing-Wing U…

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This paper evaluates and compares the performance of model-free and model-based reinforcement learning for the attitude control of fixed-wing unmanned aerial vehicles using PID as a reference point. The comparison focuses on their ability…

机器人学 · 计算机科学 2024-09-27 David Olivares , Pierre Fournier , Pavan Vasishta , Julien Marzat

Unmanned Aerial Vehicles (UAVs) will be critical infrastructural components of future smart cities. In order to operate efficiently, UAV reliability must be ensured by constant monitoring for faults and failures. To this end, the work…

信号处理 · 电气工程与系统科学 2024-04-25 Alexandre Gemayel , Dimitrios Michael Manias , Abdallah Shami

This paper introduces the powerline unmanned surfer (PLUS) concept to extend the limited endurance of fixed wing unmanned aerial vehicles (UAVs) via in-flight energy harvesting from overhead electrical distribution power lines, and develops…

系统与控制 · 电气工程与系统科学 2024-05-13 Ujjval Patel , Francis Phillips , Todd Henry , Imraan Faruque

This paper proposes a novel method for the prevention of the unbounded oscillation of an aircraft wings under the flexural torsion flutter. The paper introducing the novel multiagent method for control of an aircraft wing, assuming that the…

最优化与控制 · 数学 2021-12-14 Dmitry. S. Shalymov , Oleg N. Granichin , Yury Ivanskiy , Zeev Volkovich

It is challenging to model and control a tail-sitter unmanned aerial vehicle (UAV) because its blended wing body generates complicated nonlinear aerodynamic effects, such as wing lift, fuselage drag, and propeller-wing interactions. We…

机器人学 · 计算机科学 2023-12-25 Bailun Jiang , Boyang Li , Ching-Wei Chang , Chih-Yung Wen

Tracking position and orientation independently affords more agile maneuver for over-actuated multirotor Unmanned Aerial Vehicles (UAVs) while introducing undesired downwash effects; downwash flows generated by thrust generators may…

机器人学 · 计算机科学 2022-07-21 Yao Su , Chi Chu , Meng Wang , Jiarui Li , Liu Yang , Yixin Zhu , Hangxin Liu

Unsteady inviscid flow models of wings and airfoils have been developed to study the aerodynamics of natural and man-made flyers. Vortex methods have been extensively applied to reduce the dimensionality of these aerodynamic models, based…

流体动力学 · 物理学 2017-11-22 Xi Xia , Kamran Mohseni

As off-the-shelf (OTS) autopilots become more widely available and user-friendly and the drone market expands, safer, more efficient, and more complex motion planning and control will become necessary for fixed-wing aerial robotic…

机器人学 · 计算机科学 2018-05-24 Thomas Stastny , Roland Siegwart

Agile trajectory planning can improve the efficiency of multi-rotor Uncrewed Aerial Vehicles (UAVs) in scenarios with combined task-oriented and kinematic trajectory planning, such as monitoring spatio-temporal phenomena or intercepting…

机器人学 · 计算机科学 2025-03-19 Atharva Ghotavadekar , František Nekovář , Martin Saska , Jan Faigl

Flying animals resort to fast, large-degree-of-freedom motion of flapping wings, a key feature that distinguishes them from rotary or fixed-winged robotic fliers with limited motion of aerodynamic surfaces. However, flapping-wing…

流体动力学 · 物理学 2021-08-11 Yagiz E. Bayiz , Bo Cheng

Unmanned aircraft systems can perform some more dangerous and difficult missions than manned aircraft systems. In some highly complicated and changeable tasks, such as air combat, the maneuvering decision mechanism is required to sense the…

机器人学 · 计算机科学 2019-08-29 Zhencai Hu , Peng Gao , Fei Wang

Fixed-wing unmanned aerial vehicles (UAVs) offer endurance and efficiency but lack low-speed agility due to highly coupled dynamics. We present an end-to-end sensing-to-control pipeline that combines bio-inspired hardware, physics-informed…

机器人学 · 计算机科学 2026-03-30 Fengze Xie , Xiaozhou Fan , Jacob Schuster , Yisong Yue , Morteza Gharib

This study investigates the influence of aerofoil shape optimisation on blade aerodynamic performance under curvilinear and unsteady kinematics characteristic of vertical-axis turbines and cycloidal propellers. Using a cyclorotor in hover…

流体动力学 · 物理学 2026-03-10 Benjamin Irwin , David Toal , Swathi Krishna

We present a numerical study to characterize nonlinear unsteady aeroelastic interactions of two-dimensional flexible wings at high angles of attack. The coupled fluid-flexible wing system is solved by a body-fitted variational aeroelastic…

流体动力学 · 物理学 2023-07-07 Guojun Li , Rajeev Kumar Jaiman

This article presents a three-dimensional nonlinear trajectory tracking control strategy for unmanned aerial vehicles (UAVs) in the presence of spatial constraints. As opposed to many existing control strategies, which do not consider…

系统与控制 · 电气工程与系统科学 2024-07-16 Saurabh Kumar , Shashi Ranjan Kumar , Abhinav Sinha

Avian-informed drones feature morphing wing and tail surfaces, enhancing agility and adaptability in flight. Despite their large potential, realising their full capabilities remains challenging due to the lack of generalized control…

机器人学 · 计算机科学 2025-05-07 Simon L. Jeger , Valentin Wüest , Charbel Toumieh , Dario Floreano

In the field of fixed wing aircraft, many morphing technologies have been applied to the wing, such as adaptive airfoil, variable span aircraft, variable swept angle aircraft, etc., but few are aimed at the tail. The traditional fixed wing…

流体动力学 · 物理学 2020-10-09 Liming Zheng , Zhou Zhou , Pengbo Sun , Zhilin Zhang , Rui Wang

Hybrid unmanned aerial vehicles (UAVs) integrate the efficient forward flight of fixed-wing and vertical takeoff and landing (VTOL) capabilities of multicopter UAVs. This paper presents the modeling, control and simulation of a new type of…

机器人学 · 计算机科学 2026-01-27 Quan Quan , Wang Shuai , Gao Wenhan

This paper proposes a novel method for prevention of the increasing oscillation of an aircraft wing under the flexural torsion flutter. The paper introduces the novel multi-agent method for control of an aircraft wing, assuming that the…

信息论 · 计算机科学 2020-12-09 Dmitry S. Shalymov , Oleg N. Granichin , Zeev Volkovich , Gerhard-Wilhelm Weber

This paper deals with the estimation of the performance and stability for a shrouded-fan unmanned rotorcraft whose mission profile also prescribes the flight in ground effect. The not so simple estimation of the aerodynamic coefficients and…

经典物理 · 物理学 2009-12-17 Nicola de Divitiis