Multidisciplinary Design Optimization Approach for a Small Solid Propellant Launch Vehicle Conceptual Design Using Hybrid Simulated Annealing-Reference-Cited by-同舟云学术

Multidisciplinary Design Optimization Approach for a Small Solid Propellant Launch Vehicle Conceptual Design Using Hybrid Simulated Annealing

Published:2011-10-24 Issue: Volume:110-116 Page:4765-4771
ISSN:1662-7482
Container-title:Applied Mechanics and Materials
language:
Short-container-title:AMM

Author:

Ebrahimi Masoud¹,Roshanian Jafar¹,Barzinpour Farnaz²

Affiliation:

1. K.N.Toosi University of Technology

2. Iran University of Science and Technology

Abstract

Multidisciplinary Design Optimization (MDO) of a two-stage Small Solid Propellant Launch Vehicle (SSPLV) by simulated annealing (SA) Method is investigated. Propulsion, weight, aerodynamic (geometry) and 3degree of freedom (3DOF) trajectory simulation disciplines are used in an appropriate combination. Suitable design variables, technological-functional constraints and minimum launch weight objective function are considered. To handle constraints augmentation of constraints to cost using penalty coefficients are used. Results are compared with gradient-base method that shows the ability of SA to escape local optimums.

Publisher

Trans Tech Publications, Ltd.

Link

https://www.scientific.net/AMM.110-116.4765.pdf

Reference28 articles.

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5. Roshanian J., Jodei J., Ebrahimi m., An Automated Approach to Multidisciplinary System Design Optimization of Small Solid Propellant Launch Vehicles, , AIAA conference , china, (2006).

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