Real-time modeling of retractable self-launching glider using spreadsheets
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 2 October 2017
Abstract
Purpose
This paper aims to propose a spreadsheet method for modeling and simulation of a retraction system mechanism for the retractable self-launching system for a high-performance glider.
Design/methodology/approach
More precisely, the method is based on parametric link design using Excel spreadsheets.
Findings
This method can be used for kinematic and dynamic analysis, graphical plotting and allows simulation of control kinematics with the ability to make quick and easy parametric changes to a design. It also has the ability to calculate the loads imposed on each component in the control system as a function of input loads and position.
Practical implications
This paper shows that it is possible to model complex control systems quickly and easily using spreadsheet programs already owned by most small companies. The spreadsheet model is a parametric model, and it gives a simple visual presentation of the control system with interactive movement and control by the user.
Originality/value
This spreadsheet model in conjunction with a simple CAD program enables the rapid and cost-effective development of control system components.
Keywords
Citation
Nogoud, Y.A., Jonker, A., Mansor, S. and Abuelnuor, A.A.A. (2017), "Real-time modeling of retractable self-launching glider using spreadsheets", Aircraft Engineering and Aerospace Technology, Vol. 89 No. 6, pp. 791-796. https://doi.org/10.1108/AEAT-05-2014-0076
Publisher
:Emerald Publishing Limited
Copyright © 2017, Emerald Publishing Limited