Assessment of Drag Prediction Techniques for a Flying Vehicle Based on Radar-Tracked Data

Author:

Doso M.ORCID,Zakaria M. Y.,Ahmed Mahmoud Y. M.,Khalil Mostafa

Abstract

AbstractAs far as the aerodynamic characterization of a flying vehicle is concerned, flight testing is probably the most accurate approach as it perfectly resembles the real flight environment. Flight data are obtained by tracking the vehicle via radars if modifying the vehicle design is not recommended/attainable. In the open literature, different techniques are used to analyze radar data; the key issue is the computational demands of each technique and the quality of the resulting aerodynamic characteristics. In this paper, three techniques are considered namely, Least-Square (LS), Maximum-Likelihood Estimation (MLE), and Stepwise Regression (SR), with focus on the prediction of the drag coefficient of a case study vehicle. Features for each technique are addressed based on brief previous published data. A new variant of the MLE method is proposed based on the physical segmentation of the available dataset. Predicted point-mass trajectories are compared with own comprehensive flight test to assess the techniques in concern. It is concluded that Stepwise-regression outperforms with a large dataset, while Maximum-Likelihood Estimation is more feasible considering the lack of data. The proposed variant of the MLE method yields more accurate drag prediction compared to the basic one.

Funder

scince, tecnology and innovation funding authority

Military Technical College

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Aerospace Engineering,General Materials Science,Control and Systems Engineering

Reference43 articles.

1. McCoy R (1999) Modern exterior ballistics: the launch and flight dynamics of symmetric projectiles. ed: Schiffer Publishing Ltd

2. Whyte RH (1973) SPIN-73 an updated version of the SPINNER computer Program. General Electric Co Burlington VT Armament and Electrical Systems Dept

3. Kiran dB (2014) Drag and check predictions of the M549, 155mm Project," International Journal of Engineering Research and Reviews, vol. Volume 2, no. ISSUE3, pp. 26–33, July - September

4. McCoy RL (1981) MC DRAG-a computer program for estimating the drag coefficients of projectiles. Army Ballistic Research Lab Aberdeen Proving Ground MD

5. Champigny P, Denis P (2004) The ONERA aeroprediction code “MISSILE” ONERA: Tire a Part, no. 112, pp. 1–7

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