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APPLICATION BRIEFS

Using Response Surface Approximations to Cover Holes in the Design Space: Conceptual Design of a Missile

[+] Author and Article Information
M. Alexandra Schönning, Jamal F. Nayfeh

University of Central Florida, Mechanical Materials and Aerospace Engineering Dept., Engineering Bldg 1, Room 307, 4000 Central Florida Blvd., Orlando, FL 32816-2450

P. Richard Zarda

Lockheed Martin Missile and Fire Control - Orlando, 5600 Sand Lake Road MP 135, Orlando, FL 32819-8907

J. Comput. Inf. Sci. Eng 2(3), 224-231 (Jan 02, 2003) (8 pages) doi:10.1115/1.1527056 History: Received July 01, 2002; Revised October 01, 2002; Online January 02, 2003
Copyright © 2002 by ASME
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References

Figures

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Problem of local optimum during gradient based optimization
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Face centered full factorial central composite design
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Optimization methodology including DOE and RSA
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A hole discovered at (1, −1) and selection of new design point
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(a) Gradient-path; (b) DOE data points
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(a) Actual function and data points sampled; (b) Response surface approximation based on data points sampled
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Objective function versus iteration number
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Mass constraint versus iteration number
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(a) Desired gradient-based optimization path; (b) Gradient-based optimization path encountering a hole
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Gradient-based analysis using the Multidisciplinary Feasible formulation
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IMD disciplines and analysis codes
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Missile design being optimized

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