Aerodynamic Parameter Identification for Symmetric Projectiles: An Improved Gradient Based Method-Reference-Cited by-同舟云学术

Aerodynamic Parameter Identification for Symmetric Projectiles: An Improved Gradient Based Method

Published:2012-08-13 Issue: Volume: Page:
ISSN:
Container-title:AIAA Atmospheric Flight Mechanics Conference
language:
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Author:

Burchett Bradley¹

Affiliation:

1. Rose-Hulman Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-4861

Reference13 articles.

1. A method for extracting aerodynamic coefficients from free-flight data

2. Preliminary Model Matching of the EMBRAER 170 Jet

3. SLcp 0.295 0.296 0.34 0.257 12.9 CNA 14 13.998 0.014 10.99 21.5 CMQ -590 -535.8 9.19 -861.2 46.0

4. CLP -8.75 -10.63 21.5 -6.72 23.1 p0(1) -9.9804 -16.69 67.2 0.6069 93.9 q0(1) -0.0286 -0.0326 14.0 -0.0399 39.4 r0(1) -0.784 -0.798 1.79 -1.022 30.2 p0(2) -4.9804 -25.54 413 -17.67 255 q0(2) -0.286 -0.295 3.15 -0.375 30.9 r0(2) -0.0784 -0.0803 2.42 -0.1035 31.95 CLDD2 -0.2 -0.165 17.5 -0.141 0.1644

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