56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 2015
DOI: 10.2514/6.2015-0900
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Simultaneous aircraft allocation and mission optimization using a modular adjoint approach

Abstract: The aircraft design optimization problem is typically formulated to maximize performance at a small number of representative operating conditions. This approach makes simplifying assumptions such as ignoring the climb and descent phases, but they can be avoided by performing simultaneous designmission-allocation optimization with surrogate models for the aircraft design disciplines. As a first step towards this goal, this paper presents a method for simultaneous allocation-mission optimization. We integrate ae… Show more

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Cited by 12 publications
(11 citation statements)
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“…The first attempt to demonstrate the combined problem uses a form of branch-and-bound (BB) algorithm that enforces the integer constraints and solves only the mission-allocation problem (i.e., it ignores the aircraft design) for a simplistic three-route airline network problem [17]. For this three-route example problem, the simultaneous approach showed an improvement in the airline profit compared to the sequential approach.…”
Section: Fig 2 Sequential Decomposition Approach (Adapted From Ref mentioning
confidence: 99%
“…The first attempt to demonstrate the combined problem uses a form of branch-and-bound (BB) algorithm that enforces the integer constraints and solves only the mission-allocation problem (i.e., it ignores the aircraft design) for a simplistic three-route airline network problem [17]. For this three-route example problem, the simultaneous approach showed an improvement in the airline profit compared to the sequential approach.…”
Section: Fig 2 Sequential Decomposition Approach (Adapted From Ref mentioning
confidence: 99%
“…The first attempt to demonstrate the combined problem uses a form of Branch and Bound (BB) algorithm that enforces the integer constraints and solves only the mission-allocation problem (i.e., it ignores the aircraft design) for a simplistic three-route airline network problem [15]. For this three-route example problem, the simultaneous approach showed an improvement in the airline profit compared to the sequential approach.…”
Section: Literature Reviewmentioning
confidence: 99%
“…Compared to design-only optimization, this problem requires tens of thousands more evaluations of the aircraft performance model because of the number of mission points, the number of iterations required to converge the coupled mission analysis, and the number of routes in the airline network. A previous study outlined a method for making this problem tractable and focused on allocation-mission optimization as a starting point [1]. The proposed method would use aerostructural and propulsion surrogate models that are retrained every optimization iteration, and these surrogate models would be used for the mission analysis at much lower cost.…”
Section: Introductionmentioning
confidence: 99%
“…This framework, which uses the modular analysis and unified derivatives (MAUD) architecture [2], greatly simplified the code implementation and solution of the optimization problem. MAUD is now implemented in OpenMDAO [3], and it has been applied to the solution of allocation [1], mission [4], satellite [5], and wind turbine [6] design optimization problems.…”
Section: Introductionmentioning
confidence: 99%
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