(3.15.153.69)
Users online: 8320     
Ijournet
Email id
 

International Journal of Scientific Engineering and Technology
Year : 2013, Volume : 2, Issue : 4
First page : ( 207) Last page : ( 210)
Online ISSN : 2277-1581.

Identification of Longitudinal Aircraft Dynamics by Process Model using MATLAB/SIMULINK

Sanwale Jitu*, Singh Dhan Jeet**

Design Electrical Department, Aircraft Upgrade R&D Centre, Hindustan Aeronautics Limited, Nasik (MH)

*jituspec@iitr.ernet.in

**dhanjeet1981@rediffmail.com

Online published on 4 November, 2017.

Abstract

System-identification methods compose a mathematical model, or series of models, from measurements of inputs and outputs of dynamic systems. The estimated models allow the characterization of the response of the overall aircraft or component subsystem behavior. This paper discusses the use of System Identification Toolbox of MATLAB/SIMULINK for the estimation of aircraft flight dynamics in longitudinal channel. The data extraction, model selection and estimation of aircraft dynamics by process modeling along with data validation, time and frequency response analysis is illustrated using the system-identification simulation environment.

Top

Keywords

System Identification, Process model, MATLAB/SIMULINK.

Top

  
║ Site map ║ Privacy Policy ║ Copyright ║ Terms & Conditions ║ Page Rank Tool
746,656,236 visitor(s) since 30th May, 2005.
All rights reserved. Site designed and maintained by DIVA ENTERPRISES PVT. LTD..
Note: Please use Internet Explorer (6.0 or above). Some functionalities may not work in other browsers.