Turnitin
降AI改写
早检测系统
早降重系统
Turnitin-UK版
万方检测-期刊版
维普编辑部版
Grammarly检测
Paperpass检测
checkpass检测
PaperYY检测
Aero-propulsive modeling for tilt-wing, distributed propulsion aircraft using wind tunnel data
A high-fidelity, integrated propulsion–airframe aerodynamic model was developed for the
Langley Aerodrome No. 8 (LA-8) tandem tilt-wing, distributed electric propulsion, vertical …
Langley Aerodrome No. 8 (LA-8) tandem tilt-wing, distributed electric propulsion, vertical …
Wind tunnel-based aerodynamic model identification for a tilt-wing, distributed electric propulsion aircraft
View Video Presentation: https://doi. org/10.2514/6.2021-1298. vid This paper describes the
methodology used to develop a high-fidelity aerodynamic model for the Langley Aerodrome …
methodology used to develop a high-fidelity aerodynamic model for the Langley Aerodrome …
Attitude and cruise control of a VTOL tiltwing UAV
This letter presents the mathematical modeling, controller design, and flight testing of an
overactuated vertical take-off and landing tiltwing unmanned aerial vehicle (UAV). Based on …
overactuated vertical take-off and landing tiltwing unmanned aerial vehicle (UAV). Based on …
Nonlinear Dynamic Inversion Flight Control of a Tiltwing VTOL Aircraft
View Video Presentation: https://doi. org/10.2514/6.2023-1910. vid This paper explores
dynamic inversion-based flight control applied to a tiltwing vertical take-off and landing …
dynamic inversion-based flight control applied to a tiltwing vertical take-off and landing …
Unified incremental nonlinear controller for the transition control of a hybrid dual-axis tilting rotor quad-plane
Hybrid overactuated tilt rotor uncrewed aerial vehicles (TRUAVs) are a category of versatile
UAVs known for their exceptional wind resistance capabilities. However, their extensive …
UAVs known for their exceptional wind resistance capabilities. However, their extensive …
H∞ Robust Control of a Quadrotor Biplane Tailsitter UAV
Environmental disturbances, nonlinearities, and system uncertainties frequently impact the
stability and performance of unmanned aerial vehicles (UAVs). This research proposes a …
stability and performance of unmanned aerial vehicles (UAVs). This research proposes a …
Robust H-infinity control for a quadrotor UAV
View Video Presentation: https://doi. org/10.2514/6.2022-2033. vid The different types of
uncertainties and non-linearities found in the quadrotor's model necessitate the …
uncertainties and non-linearities found in the quadrotor's model necessitate the …
Advances in Aero-Propulsive Modeling for Fixed-Wing and eVTOL Aircraft Using Experimental Data
BM Simmons - 2023 - vtechworks.lib.vt.edu
Small unmanned aircraft and electric vertical takeoff and landing (eVTOL) aircraft have
recently emerged as vehicles able to perform new missions and stimulate future air …
recently emerged as vehicles able to perform new missions and stimulate future air …
Optimized Sliding Mode Control via Genetic Algorithm for Quad Tilt-Wing UAVs
In the ever-evolving landscape of unmanned aerial vehicles (UAVs), the focus of this paper
is on enhancing the performance and control of a Quad-Titl wing UAV (QTWUAV). QTW …
is on enhancing the performance and control of a Quad-Titl wing UAV (QTWUAV). QTW …
Flight mechanics and control of tilt rotor/tilt wing unmanned aerial vehicles: A review
A literature review of the Tilt Rotor/Tilt Wing (TR/TW) Unmanned Aerial Vehicles (UAVs) is
presented in this paper from the flight mechanics and control points of view. Firstly, the …
presented in this paper from the flight mechanics and control points of view. Firstly, the …