2020
DOI: 10.1016/j.asoc.2020.106665
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A physics-aware learning architecture with input transfer networks for predictive modeling

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Cited by 10 publications
(8 citation statements)
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“…To address these issues, a novel hybrid architecture was introduced by Behjat et al [25] which uses partial physics as an additional node in the model. This model was called "Opportunistic Physics-mining Transfer Mapping Architecture" or OPTMA, and it was used in a dynamics prediction problem, for UAV flight prediction under gust [26]; and in a CFD simulation modeling problem, to explore bio-inspired surface riblets for drag Reduction [27]. While OPTMA outperformed data-driven and classical hybrid architectures, it was challenging to train it in a gradient-based way without generating the labels.…”
Section: A Physics-infused Hybrid Modelingmentioning
confidence: 99%
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“…To address these issues, a novel hybrid architecture was introduced by Behjat et al [25] which uses partial physics as an additional node in the model. This model was called "Opportunistic Physics-mining Transfer Mapping Architecture" or OPTMA, and it was used in a dynamics prediction problem, for UAV flight prediction under gust [26]; and in a CFD simulation modeling problem, to explore bio-inspired surface riblets for drag Reduction [27]. While OPTMA outperformed data-driven and classical hybrid architectures, it was challenging to train it in a gradient-based way without generating the labels.…”
Section: A Physics-infused Hybrid Modelingmentioning
confidence: 99%
“…Previously, Particle Swarm Optimization has been used to train OPTMA [26]. This is however, computationally very expensive and would not be viable for complex physics-based models.…”
Section: A Previous Frameworkmentioning
confidence: 99%
“…where L is the lift, D is the drag, W is the aircraft weight, and Th is the thrust. Equation (12) denotes that thrust required is the drag, and equals to the following aerodynamic equation:…”
Section: Cruise Fuel Consumption Dynamicsmentioning
confidence: 99%
“…The Mach number distribution is skewed, and most of the population is around 0.83, which is usually the nominal cruise speed regime for this aircraft. For a greater gross weight, an autopilot system sets throttle to a higher position to maintain Equation (12). Figure 6 depicts gross weight correlation with the throttle δ T , and fuel consumption from data.…”
Section: Cruise Fuel Consumption Dynamicsmentioning
confidence: 99%
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