Mathematical Model for Studying the Evolution of Multi-Role Unmanned Aerial Vehicle in Turbulent Atmosphere

Cristina Mihailescu; Ioan Farcasan

doi:10.4028/www.scientific.net/AMM.325-326.984

Paper Titles

A New Mechanical Moving Device Based on the Polarization Navigation Method
p.956

Power Split Strategy of Plug-in Series Hybrid Electric Bus Based on Fuzzy Control
p.961

Modeling and Simulation of a Small-Scale Mining Road Headers Constant Power System
p.966

Assisted Optimization of the Servo Driving by Using Virtual Labview Instrumentation and the Elementary Transfer Functions and Neural Network Methods
p.970

Mathematical Model for Studying the Evolution of Multi-Role Unmanned Aerial Vehicle in Turbulent Atmosphere
p.984

First Flight Experiment with the NERVA-1 Inertial Platform
p.990

Modelling and Control of a Star-Shaped Octorotor
p.994

Simulation of Manipulator with Flexible Joint
p.999

The Accurate Calculation Model of Vector Azimuth Based on DTG
p.1004

HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 325-326Mathematical Model for Studying the Evolution of...

Mathematical Model for Studying the Evolution of Multi-Role Unmanned Aerial Vehicle in Turbulent Atmosphere

Abstract:

The paper purpose is to present some aspects regarding the control system of unmanned aerial vehicle - UAV, used for local observations, surveillance and monitoring of interest area or as a training target for anti-aircraft systems. The calculus methodology allows a numerical simulation of UAV evolution in bad atmospheric conditions by using a nonlinear model, as well as a linear one for obtaining the guidance command. The UAV model which will be presented has six DOF (degrees of freedom), and an autonomous control system. This theoretical development allows us to build the stability matrix, command matrix and the control matrix and finally to analyze the stability of autonomous UAV flight. A robust guidance system, based on Kalman filter will be evaluated for different fly conditions and the results will be presented. The flight parameters and guidance will be analyzed. The paper is inspired by national project SAMO (Autonomous Aerial Monitoring System for Interest Areas of Great Endurance). Keywords: UAV, Simulation, Control, Guidance, Endurance, Surveillance, Monitoring, Kalman filter

You might also be interested in these eBooks

Manufacturing Engineering and Process II

View Preview

Info:

Periodical:

Applied Mechanics and Materials (Volumes 325-326)

Pages:

984-989

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.325-326.984

Citation:

Cite this paper

Online since:

June 2013

Authors:

Cristina Mihailescu, Ioan Farcasan

Keywords:

Control, Endurance, Guidance, Kalman Filter (KF), Monitoring, Simulation, Surveillance, UAV

Export:

RIS, BibTeX

Price:

Permissions:

Request Permissions

References

[1] Bakhvalov, N. Methodes Numeriques – Analyse, algebre, equations differentielles ordinaires, Moscou,(1976)

Google Scholar

[2] Bandu N. P. Performance, Stability, Dynamics and Control of Airplanes Second Edition, AIAA Education Series, ISBN 1-56347-583-9, 2003.

Google Scholar

[3] Boiffier, J.L. The Dynamics of Flight – The Equations, John Wiley & Sons , Chichester, New York, Weinheim, Brisbane, Singapore, Toronto , ISBN 0-471-94237-5, 1998.

DOI: 10.1002/abio.370180404

Google Scholar

[4] Chelaru T.V., Constantinescu V.N., Chelaru A., Control system of unmanned aerial vehicle used for endurance autonomous monitoring WSEAS TRANSACTIONS on SYSTEMS and CONTROL, ISSN: 1991-8763, pp.767-778, Issue 9, Volume 5, September 2010.

DOI: 10.1063/1.4904578

Google Scholar

[5] Chelaru T.V. Constantinescu N.V, Chelaru A., Mathematic model and technical solution for surveillance and autonomous monitoring system based on endurance unmanned aerial vehicle, Proceedings of 11th WSEAS Int. Conf. on Automation & Information (ICAI'10), pp.149-155, ISBN 978-960-474-193-9, ISSN 1790-5117, University of G.Enescu, Iasi, Romania, June 13-15, 2010.

DOI: 10.1063/1.4904578

Google Scholar

[6] Chelaru T.V. Cnstantinescu V.N, Popa E., Chelaru A., Unmanned aerial vehicle for surveillance and autonomous monitoring costal area, Proceedings of the the 3rd International Conference on MARITIME and NAVAL SCIENCE and ENGINEERING (MN'10), pp.227-232, ISBN: 978-960-474-222-6, ISSN: 1792-4707,Constanta Maritime University, Constanta, Romania, September 3-5, 2010.

DOI: 10.53464/jmte.01.2022.09

Google Scholar

[7] Etkin, B., Dinamics of Atmospheric Flight, John Wiley & Sons, Inc., New York, 1972.

Google Scholar

[8] Nita, M.M., Moraru, Fl., Patraulea, R., Avioane şi rachete, concepte de proiectare, Ed. Militara, Bucuresti, 1985.

Google Scholar