Co-simulation of matlab and flightgear for identification and control of aircraft

G Aschauer, A Schirrer, M Kozek - IFAC-PapersOnLine, 2015 - Elsevier
The paper outlines the development of a co-simulation solution of Matlab and Flight-Gear in
which the communication between these programs is done via UDP without needing further …

[PDF][PDF] 飞翼布局飞行器容错控制可视化仿真平台开发

张绍杰, 孟庆开 - 系统仿真学报, 2018 - china-simulation.com
针对某型飞翼布局飞行器的容错飞行控制可视化仿真验证问题, 开发了一个基于QtQuick
的仿真平台. 使用Simulink 搭建飞行器数学模型及容错飞行控制律, 作为可视化平台模型驱动端 …

Design of Fault Tolerant Control Visual Simulation System For Flying Wing Aircrafts

S Zhang, Q Meng - Journal of System Simulation, 2019 - dc-china-simulation …
A visual simulation platform based on Qt Quick was designed with respect to the simulation
about fault tolerant control for flying wing aircrafts. Aircraft mathematical model and control …

Enhancement of light aircraft 6 DOF simulation using flight test data in longitudinal motion

LVT Nguyen, M Tyan, JW Lee, S Kim - The Aeronautical Journal, 2021 - cambridge.org
This paper proposes a procedure to improve the accuracy of the light aircraft 6 DOF
simulation model by implementing model tuning and aerodynamic database correction …

APRICOT: Aerospace prototyping control toolbox. A modeling and simulation environment for aircraft control design

A Ferrarelli, D Caporale, A Settimi… - Modelling and Simulation …, 2016 - Springer
A novel MATLAB/Simulink based modeling and simulation environment for the design and
rapid prototyping of state-of-the-art aircraft control systems is proposed. The toolbox, named …

[PDF][PDF] Implementation of a washout filter used in Stewart platform

RC Lemes, R Breganon, MM Souza, FTB Salvi… - COBEM …, 2015 - academia.edu
The aim of this work is to implement the filter called Classic Washout, which creates
sensations of movement, for application in a movable Stewart platform. This washout filter is …

Modelamiento Dinámico de los Parametros de Control de Vuelo de una Aeronave del Tipo ala Volante Utilizando Redes Neuronales Artificiales

CS Villanueva - 2018 - search.proquest.com
Esta tesis de investigación propone obtener el modelo aerodinámico de una aeronave del
tipo ala volante utilizando redes neuronales artificiales con el fin de mejorar la performance …

Modelamiento dinámico de los parametros de control de vuelo de una aeronave del tipo ala volante utilizando redes neuronales artificiales.

C Saito Villanueva - 2018 - tesis.pucp.edu.pe
Esta tesis de investigación propone obtener el modelo aerodinámico de una aeronave del
tipo ala volante utilizando redes neuronales artificiales con el fin de mejorar la performance …

[引用][C] 平流层演示验证飞艇实时仿真平台设计

惠光飞, 陈丽, 段登平 - 计算机仿真, 2013