NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Optimal Control within the Context of Multidisciplinary Design, Analysis, and OptimizationMultidisciplinary design, analysis and optimization involves modeling the interactions of complex systems across a variety of disciplines. The optimization of such systems can be a computationally expensive exercise with multiple levels of nested nonlinear solvers running under an optimizer.The application of optimal control in project development often involves performing trajectory optimization for fixed vehicle designs or parametric sweeps across some key vehicle properties.This information is then relayed to the subsystem design teams who update their designs and relay some bulk characteristics back to the trajectory optimization procedure.This iteration is then repeated until the design closes.However, with increasing interest in more tightly coupled systems, such as electric and hybrid-electric aircraft propulsion and boundary layer ingestion, this process is prone to ignore subtle coupling between vehicle subsystem designs and vehicle operation on a given mission.Integrating trajectory optimization into a tightly coupled multidisciplinary design procedure can be computationally prohibitive, depending on the complexity of the subsystem analyses and the optimal control technique applied.To address these issues a new optimal control software tool, Dymos, has been developed.Dymos is built upon NASA's OpenMDAO software and can leverage its capabilities to efficiently compute gradients for the optimization and optimize complex models in parallel on distributed memory systems.This report provides some explanation into the numerical methods employed in Dymos and provides several use cases that demonstrate its performance on traditional optimal control problems and improvements ino techniques have been used extensively in recent decades to solve a variety of optimal control problems, typically in the form of aerospace vehicle trajectory optimization.
Document ID
20190002793
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Falck, Robert D.
(NASA Glenn Research Center Cleveland, OH, United States)
Gray, Justin S.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
April 26, 2019
Publication Date
January 7, 2019
Subject Category
Aircraft Design, Testing And Performance
Computer Programming And Software
Report/Patent Number
GRC-E-DAA-TN63527
Meeting Information
Meeting: 2019 American Institute of Aeronautics and Astronautics (AIAA) SciTech Forum
Location: San Diego, CA
Country: United States
Start Date: January 7, 2019
End Date: January 11, 2019
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)
Funding Number(s)
WBS: 109492.02.03.01.10.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
pseudospectral
No Preview Available