Optimization under Uncertainty Techniques for Time-Dependent Aircraft Systems with Controllers

DL Clark, CT Aksland, CA Lupp… - AIAA SCITECH 2023 …, 2023 - arc.aiaa.org
AIAA SCITECH 2023 Forum, 2023arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-1095. vid This paper explores
intrusive and non-intrusive methods that enable the inclusion of stochastic differential
equations in design optimization of time-dependent systems. Using a gradient-based
trajectory optimization formulation, pseudospectral integration, and proportional-integral
controllers, uncertainties are introduced through distributed initial conditions, material
properties, and performance coefficients, and are mitigated by changing open-loop control …
View Video Presentation: https://doi.org/10.2514/6.2023-1095.vid
This paper explores intrusive and non-intrusive methods that enable the inclusion of stochastic differential equations in design optimization of time-dependent systems. Using a gradient-based trajectory optimization formulation, pseudospectral integration, and proportional-integral controllers, uncertainties are introduced through distributed initial conditions, material properties, and performance coefficients, and are mitigated by changing open-loop control inputs or closed-loop controller gains. The examples include a linear system for uncertainty propagation and open-loop control optimization, and reproducible polyalphaolefin mixing chamber for optimal control gain selection. The linear system provides a fundamental baseline and the mixing chamber is simple enough for others to easily implement. The methods under investigation include Monte Carlo simulation, intrusive and non-intrusive generalized polynomial chaos, and unscented transform.
AIAA Aerospace Research Center
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