Design and Implementation of a Hardware‐in‐the‐Loop Simulation System for a Tilt Trirotor UAV

L Yu, G He, S Zhao, X Wang… - Journal of Advanced …, 2020 - Wiley Online Library
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 …

A Neural Autopilot Training Platform based on a Matlab and X-Plane co-simulation

J Pinguet, P Feyel, G Sandou - 2021 International Conference …, 2021 - ieeexplore.ieee.org
The main objective of this paper is to describe a tool for the aircraft autopilot deployment
only based on a flight database. Flight simulators such as X-Plane turn out to be powerful …

System identification flight testing of inverted v-tail small unmanned air system

CJ Leshikar, S Gosnell, E Gomez, L Moy… - AIAA SciTech 2022 …, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-2408. vid This paper presents an
approach for generating linear time invariant state-space models of a small Unmanned Air …

Incremental adaptive fixed‐wing unmanned aerial vehicle maneuver control with nonlinear disturbance observer: A finite‐time approach

S Cao, X Wang, H Yu - Asian Journal of Control, 2023 - Wiley Online Library
This article proposes a versatile controller based on the incremental strategy to explore a
finite‐time (FT) solution of fixed‐wing unmanned aerial vehicle (UAV) maneuver control …

Software in-loop simulation of a quad tilt rotor unmanned aerial vehicle for transition control

S Elanchezhian - Transactions of FAMENA, 2023 - hrcak.srce.hr
Sažetak This paper presents a hybrid unmanned aerial vehicle configuration, the quad tilt
rotor (QTR), which combines both the tandem wing configuration and the quadrotor …

Comparison of black-grey-white box approach in system identification of a flight vehicle

L Nugroho, R Akmeliawati - Journal of Physics: Conference …, 2018 - iopscience.iop.org
Developing an autonomous flight control system for a fixed-wing unmanned aerial vehicle
(UAV) requires the mathematical representation of the system dynamics which can be …

Optimal bearing-only-information strategy for unmanned aircraft collision avoidance

TL Molloy, T Perez, BP Williams - Journal of Guidance, Control, and …, 2020 - arc.aiaa.org
This paper presents a novel collision-avoidance strategy for unmanned aircraft detect and
avoid that requires only information about the relative bearing angle between an aircraft and …

Longitudinal aerodynamic modeling of a reduced-scale aircraft using neuro-fuzzy hybridized with differential evolution

V Sant'Ana, I Staack, RF Neto - Journal of the Brazilian Society of …, 2024 - Springer
This paper introduces a novel system identification method designed to derive detailed
unsteady aerodynamic models from aircraft measurement data, tailored specifically for …

Mathematical model derivation of an unmanned circulation control aerial vehicle UC2AV

M Agha, K Kanistras, MJ Rutherford… - Control Theory and …, 2020 - Springer
This paper presents a system identification method to derive accurate mathematical models
for an unmanned circulation control aerial vehicle (UC 2 AV) that account for the effects of …

A controller design framework for a NextGen circulation control based UAV

MG Michailidis, M Agha, K Kanistras… - … IEEE Conference on …, 2017 - ieeexplore.ieee.org
Circulation Control (CC) is an active flow blowing technique that can be used on small scale
fixed-wing Unmanned Aerial Vehicles (UAVs) to enhance lift and aerodynamic efficiency …