Flight Dynamics Model of Bombardier Global 5000 Aircraft

Mohammad Moallemi; Shafagh Jafer; Massood Towhidnejad

doi:10.2514/6.2016-3525

Flight Dynamics Model of Bombardier Global 5000 Aircraft

Mohammad Moallemi, Shafagh Jafer, Massood Towhidnejad

Embry-Riddle Aeronautical University - Daytona Beach

Research output: Contribution to conference › Presentation

Abstract

"This paper focuses on modeling the flight dynamics a Bombardier Global 5000 (BD-700-1A11) deploying a discrete-time simulation methodology. The goal is to develop a medium-fidelity Flight Dynamic Model (FDM) of this aircraft to be deployed in a desktop flight simulator in the Next Generation Applied Research (NEAR) lab at Embry-Riddle Aeronautical University for validation of the future air traffic management concepts and control technologies. The model was designed using publicly available aircraft data. The design was implemented using JSBSim open-source flight dynamics modeler. The aircraft FDM, the engine forces, and the autopilot were developed in JSBSim and tested using fast-time simulation under different scenarios. Aircraft operational limits as well as operational flight manual published by the manufacturer have been used to validate the FDM properties and maneuverability. The results of the initial tests are presented in this paper."--From the paper.

Original language	American English
DOIs	https://doi.org/10.2514/6.2016-3525
State	Published - Jun 2016
Externally published	Yes
Event	AIAA Modeling and Simulation Technologies Conference - Washington, DC Duration: Jun 1 2016 → …

Conference

Conference	AIAA Modeling and Simulation Technologies Conference
Period	6/1/16 → …

Keywords

simulation
desktop flight simulator
flight dynamics modeler

Disciplines

Aviation
Other Electrical and Computer Engineering

Access to Document

10.2514/6.2016-3525License: Unspecified

Cite this

@conference{4c12383c1c01488db7637330d408607d,

title = "Flight Dynamics Model of Bombardier Global 5000 Aircraft",

abstract = " {"}This paper focuses on modeling the flight dynamics a Bombardier Global 5000 (BD-700-1A11) deploying a discrete-time simulation methodology. The goal is to develop a medium-fidelity Flight Dynamic Model (FDM) of this aircraft to be deployed in a desktop flight simulator in the Next Generation Applied Research (NEAR) lab at Embry-Riddle Aeronautical University for validation of the future air traffic management concepts and control technologies. The model was designed using publicly available aircraft data. The design was implemented using JSBSim open-source flight dynamics modeler. The aircraft FDM, the engine forces, and the autopilot were developed in JSBSim and tested using fast-time simulation under different scenarios. Aircraft operational limits as well as operational flight manual published by the manufacturer have been used to validate the FDM properties and maneuverability. The results of the initial tests are presented in this paper.{"}--From the paper. ",

keywords = "simulation, desktop flight simulator, flight dynamics modeler",

author = "Mohammad Moallemi and Shafagh Jafer and Massood Towhidnejad",

year = "2016",

month = jun,

doi = "10.2514/6.2016-3525",

language = "American English",

note = "AIAA Modeling and Simulation Technologies Conference ; Conference date: 01-06-2016",

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TY - CONF

T1 - Flight Dynamics Model of Bombardier Global 5000 Aircraft

AU - Moallemi, Mohammad

AU - Jafer, Shafagh

AU - Towhidnejad, Massood

PY - 2016/6

Y1 - 2016/6

N2 - "This paper focuses on modeling the flight dynamics a Bombardier Global 5000 (BD-700-1A11) deploying a discrete-time simulation methodology. The goal is to develop a medium-fidelity Flight Dynamic Model (FDM) of this aircraft to be deployed in a desktop flight simulator in the Next Generation Applied Research (NEAR) lab at Embry-Riddle Aeronautical University for validation of the future air traffic management concepts and control technologies. The model was designed using publicly available aircraft data. The design was implemented using JSBSim open-source flight dynamics modeler. The aircraft FDM, the engine forces, and the autopilot were developed in JSBSim and tested using fast-time simulation under different scenarios. Aircraft operational limits as well as operational flight manual published by the manufacturer have been used to validate the FDM properties and maneuverability. The results of the initial tests are presented in this paper."--From the paper.

AB - "This paper focuses on modeling the flight dynamics a Bombardier Global 5000 (BD-700-1A11) deploying a discrete-time simulation methodology. The goal is to develop a medium-fidelity Flight Dynamic Model (FDM) of this aircraft to be deployed in a desktop flight simulator in the Next Generation Applied Research (NEAR) lab at Embry-Riddle Aeronautical University for validation of the future air traffic management concepts and control technologies. The model was designed using publicly available aircraft data. The design was implemented using JSBSim open-source flight dynamics modeler. The aircraft FDM, the engine forces, and the autopilot were developed in JSBSim and tested using fast-time simulation under different scenarios. Aircraft operational limits as well as operational flight manual published by the manufacturer have been used to validate the FDM properties and maneuverability. The results of the initial tests are presented in this paper."--From the paper.

KW - simulation

KW - desktop flight simulator

KW - flight dynamics modeler

U2 - 10.2514/6.2016-3525

DO - 10.2514/6.2016-3525

M3 - Presentation

T2 - AIAA Modeling and Simulation Technologies Conference

Y2 - 1 June 2016

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