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相关论文: Adaptive Nonlinear Control of Fixed-Wing VTOL with…

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We propose a method to generate robust and optimal trajectories for the transition of a tiltwing Vertical Take-Off and Landing (VTOL) aircraft leveraging concepts from convex optimisation, tube-based nonlinear Model Predictive Control (MPC)…

最优化与控制 · 数学 2023-02-10 Martin Doff-Sotta , Mark Cannon , Marko Bacic

In this paper, an adaptive super-twisting controller is designed for an agile maneuvering quadrotor unmanned aerial vehicle to achieve accurate trajectory tracking in the presence of external disturbances. A cascaded control architecture is…

系统与控制 · 电气工程与系统科学 2023-09-15 D. M. K. K. Venkateswara Rao , Hamed Habibi , Jose Luis Sanchez-Lopez , Prathyush P. Menon , Christopher Edwards , Holger Voos

This paper proposes a novel observer-based controller for Vertical Take-Off and Landing (VTOL) Unmanned Aerial Vehicle (UAV) designed to directly receive measurements from a Vision-Aided Inertial Navigation System (VA-INS) and produce the…

机器人学 · 计算机科学 2023-08-28 Hashim A. Hashim , Abdelrahman E. E. Eltoukhy , Akos Odry

Two configurations typical of fixed-wing aircraft are simulated with the actuator line method (ALM): a wing with winglets and a T-tail. The ALM is extensively used in rotor simulations to model the blades by body forces, which are…

流体动力学 · 物理学 2023-03-21 Vitor G. Kleine , Ardeshir Hanifi , Dan S. Henningson

This paper presents a novel VTOL UAV that owns a link connecting four rotors and a fuselage by a passive joint, allowing the control of the rotor's tilting angle by adjusting the rotors' thrust. This unique structure contributes to…

系统与控制 · 电气工程与系统科学 2025-02-26 Takumi Ito , Riku Funada , Mitsuji Sampei

A control design approach to achieve fully autonomous take-off and flight maneuvers with a tethered aircraft is presented and demonstrated in real-world flight tests with a small-scale prototype. A ground station equipped with a controlled…

系统与控制 · 计算机科学 2017-02-17 Lorenzo Fagiano , Eric Nguyen-Van , Felix Rager , Stephan Schnez , Christian Ohler

This paper is an addition to an article previously published by three of the authors that addresses the control of convertible fixed-wing aircraft with vectorized thrust. The control solution here developed extends the one presented in the…

系统与控制 · 电气工程与系统科学 2023-11-28 Tomas Lopes de Oliveira , Andre Anglade , Tarek Hamel , Claude Samson

This paper presents a nonlinear control law for the stabilization of a fixed-wing UAV. Such controller solves the path-following problem and the longitudinal control problem in a single control. Furthermore, the control design is performed…

系统与控制 · 计算机科学 2019-03-12 Gerardo Flores , Alejandro Flores , Andrés Montes de Oca

The paper discusses a novel vision-based estimation and control approach to enable fully autonomous tracking and landing of vertical take-off and landing (VTOL) capable unmanned aerial vehicles (UAVs) on moving platforms without relying on…

机器人学 · 计算机科学 2020-08-18 Bochan Lee , Vishnu Saj , Moble Benedict , Dileep Kalathil

Tilt rotor aircraft combine the benefits of both helicopters and fixed wing aircraft, this makes them popular for a variety of applications, including Search and Rescue and VVIP transport. However, due to the multiple flight modes,…

系统与控制 · 电气工程与系统科学 2024-11-13 William Smith , Xinhua Wang

In the evolving landscape of high-speed agile quadrotor flight, achieving precise trajectory tracking at the platform's operational limits is paramount. Controllers must handle actuator constraints, exhibit robustness to disturbances, and…

机器人学 · 计算机科学 2025-10-15 Lukas Pries , Markus Ryll

A tethered multirotor autogyro can function as an unmanned aerial vehicle for energy-efficient and prolonged deployment, as it uses the available wind energy to sustain flight. This article presents an adaptive altitude control strategy for…

系统与控制 · 电气工程与系统科学 2025-09-26 Tasnia Noboni , Tuhin Das

The autonomous operation of flexible-wing aircraft is technically challenging and has never been presented within literature. The lack of an exact modeling framework is due to the complex nonlinear aerodynamic relationships governed by the…

系统与控制 · 电气工程与系统科学 2021-03-31 Mohammed Abouheaf , Nathaniel Mailhot , Wail Gueaieb , Davide Spinello

This paper investigates the coordinated trajectory tracking problem of multiple vertical takeooff and landing (VTOL) unmanned aerial vehicles (UAVs). The case of unidirectional information flow is considered and the objective is to drive…

系统与控制 · 计算机科学 2017-11-10 Yao Zou , Ziyang Meng

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 describes the design process for developing a nonlinear model predictive controller for fault tolerant flight control. After examining and implementing a number of numerical techniques, this paper identifies pseudospectral…

最优化与控制 · 数学 2016-10-10 Rudaba Khan , Paul Williams , Paul Riseborough , Asha Rao , Robin Hill

This paper presents a feedback/feedforward nonlinear controller for variable-speed wind turbines with doubly fed induction generators. By appropriately adjusting the rotor voltages and the blade pitch angle, the controller simultaneously…

最优化与控制 · 数学 2016-11-17 Choon Yik Tang , Yi Guo , John N. Jiang

Offering vertical take-off and landing (VTOL) capabilities and the ability to travel great distances are crucial for Urban Air Mobility (UAM) vehicles. These capabilities make hybrid VTOLs the clear front-runners among UAM platforms. On the…

机器人学 · 计算机科学 2022-06-02 Mohammadreza Mousaei , Azarakhsh Keipour , Junyi Geng , Sebastian Scherer

Aeroelastic structures, from insect wings to wind turbine blades, experience transient unsteady aerodynamic loads that are coupled to their motion. Effective real-time control of flexible structures relies on accurate and efficient…

流体动力学 · 物理学 2022-07-14 Michelle Hickner , Urban Fasel , Aditya G. Nair , Bingni W. Brunton , Steven L. Brunton

This paper investigates the robust nonlinear close formation control problem. It aims to achieve precise position control at dynamic flight operation for a follower aircraft under the aerodynamic impact due to the trailing vortices…

系统与控制 · 计算机科学 2019-04-17 Qingrui Zhang , Hugh H. T. Liu