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The Application of Sequential Convex Programming to Large-Scale Structural Optimization Problems

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TLDR
The largest of the three models, which had 1527 design variables and 6124 constraints, was solved to optimality with ASTROS for the first time using a mathematical programming method.
Abstract
: Structural design problems are often modeled using finite element methods. Such models are often characterized by constraint functions that are not explicitly defined in terms of the design variables. These functions are typically evaluated through numerical finite element analysis (FEA). Optimizing large-scale structural design models requires computationally expensive FEAs to obtain function and gradient values. An optimization approach which uses the SCP sequential convex programming algorithm of Zillober, integrated as the optimizer in the Automated Structural Optimization System (ASTROS), is tested. The traditional approach forms an explicitly defined approximate subproblem at each design iteration that is solved using the method of modified feasible directions. In an alternative approach, the SCP subroutine is called to formulate and solve the approximate subproblem. The SCP method is an implementation of the Method of Moving Asymptotes algorithm with five different asymptote determination strategies. This study investigates the effect of different asymptote determination strategies and constraint retention strategies on computational efficiency. The approach is tested on three large-scale structural design models, including one with constraints from multiple disciplines. Results and comparisons to the traditional approach are given. The largest of the three models, which had 1527 design variables and 6124 constraints, was solved to optimality with ASTROS for the first time using a mathematical programming method. The structural weight of the resulting design is 9% lower than the previously recorded minimum weight.

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Journal ArticleDOI

Optimal Design of a Hexakis Icosahedron Vacuum-Based Lighter-Than-Air Vehicle

Joseph R Schwemmer
- 07 May 2018 - 
TL;DR: In this article, the authors used an internal vacuum to reduce the buoyancy of a lighter-than-air (L2A) vehicle, which was used to reduce its cost and scarcity of helium.

Optimal control of fully routed air traffic in the presence of uncertainty and kinodynamic constraints

TL;DR: The methods developed and tested throughout this dissertation demonstrate the ability of graph-based optimization techniques to model realistic air traffic restrictions and generate viable control strategies.
References
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Journal ArticleDOI

Optimal Design of a Hexakis Icosahedron Vacuum-Based Lighter-Than-Air Vehicle

Joseph R Schwemmer
- 07 May 2018 - 
TL;DR: In this article, the authors used an internal vacuum to reduce the buoyancy of a lighter-than-air (L2A) vehicle, which was used to reduce its cost and scarcity of helium.

Optimal control of fully routed air traffic in the presence of uncertainty and kinodynamic constraints

TL;DR: The methods developed and tested throughout this dissertation demonstrate the ability of graph-based optimization techniques to model realistic air traffic restrictions and generate viable control strategies.
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