Javascript must be enabled to continue!
Vortex gust mitigation from onboard measurements using deep reinforcement learning
View through CrossRef
Abstract
This paper proposes to solve the vortex gust mitigation problem on a 2D, thin flat plate using onboard measurements. The objective is to solve the discrete-time optimal control problem of finding the pitch rate sequence that minimizes the lift perturbation, that is, the criterion
where
is the lift coefficient obtained by the unsteady vortex lattice method. The controller is modeled as an artificial neural network, and it is trained to minimize
using deep reinforcement learning (DRL). To be optimal, we show that the controller must take as inputs the locations and circulations of the gust vortices, but these quantities are not directly observable from the onboard sensors. We therefore propose to use a Kalman particle filter (KPF) to estimate the gust vortices online from the onboard measurements. The reconstructed input is then used by the controller to calculate the appropriate pitch rate. We evaluate the performance of this method for gusts composed of one to five vortices. Our results show that (i) controllers deployed with full knowledge of the vortices are able to mitigate efficiently the lift disturbance induced by the gusts, (ii) the KPF performs well in reconstructing gusts composed of less than three vortices, but shows more contrasted results in the reconstruction of gusts composed of more vortices, and (iii) adding a KPF to the controller recovers a significant part of the performance loss due to the unobservable gust vortices.
Cambridge University Press (CUP)
Title: Vortex gust mitigation from onboard measurements using deep reinforcement learning
Description:
Abstract
This paper proposes to solve the vortex gust mitigation problem on a 2D, thin flat plate using onboard measurements.
The objective is to solve the discrete-time optimal control problem of finding the pitch rate sequence that minimizes the lift perturbation, that is, the criterion
where
is the lift coefficient obtained by the unsteady vortex lattice method.
The controller is modeled as an artificial neural network, and it is trained to minimize
using deep reinforcement learning (DRL).
To be optimal, we show that the controller must take as inputs the locations and circulations of the gust vortices, but these quantities are not directly observable from the onboard sensors.
We therefore propose to use a Kalman particle filter (KPF) to estimate the gust vortices online from the onboard measurements.
The reconstructed input is then used by the controller to calculate the appropriate pitch rate.
We evaluate the performance of this method for gusts composed of one to five vortices.
Our results show that (i) controllers deployed with full knowledge of the vortices are able to mitigate efficiently the lift disturbance induced by the gusts, (ii) the KPF performs well in reconstructing gusts composed of less than three vortices, but shows more contrasted results in the reconstruction of gusts composed of more vortices, and (iii) adding a KPF to the controller recovers a significant part of the performance loss due to the unobservable gust vortices.
Related Results
Study of Gust Calculation and Gust Alleviation: Simulations and Wind Tunnel Tests
Study of Gust Calculation and Gust Alleviation: Simulations and Wind Tunnel Tests
Feedforward gust alleviation control using gusts as input signals has received increasing attention in recent years. One of the most important issues in such a control scheme is ho...
Investigation of vortex in pump sump by V3V measurements
Investigation of vortex in pump sump by V3V measurements
Abstract
The aims, scope and conclusions of the paper must be in a self-contained abstract of a single paragraph with 60-120 words. The abstract must be informative ...
Numerical simulation for axis switching of pulsating jet issued from rectangular nozzle at low Reynolds number
Numerical simulation for axis switching of pulsating jet issued from rectangular nozzle at low Reynolds number
Axis switching of a jet ejected from a rectangular nozzle affects flow mixing characteristics. To elucidate such a mixing mechanism, the axis switching and vortex structure deforma...
Effect of Blade Thickness on High Frequency Gust Response
Effect of Blade Thickness on High Frequency Gust Response
Turbomachinery rotor blades experience gust loading due to both inflow turbulence and circumferential variation in the mean velocity. The unsteady lift forces that result from thes...
Selection of Injectable Drug Product Composition using Machine Learning Models (Preprint)
Selection of Injectable Drug Product Composition using Machine Learning Models (Preprint)
BACKGROUND
As of July 2020, a Web of Science search of “machine learning (ML)” nested within the search of “pharmacokinetics or pharmacodynamics” yielded over 100...
Local energy of magnetic vortex core reversal
Local energy of magnetic vortex core reversal
The polarity of magnetic vortex core can be switched by current or magnetic field through a vortex-antivortex pair creation and annihilation process, in which the significant chang...
Effects of Vortex-Vortex Interaction in a Compressor Cascade With Vortex Generators
Effects of Vortex-Vortex Interaction in a Compressor Cascade With Vortex Generators
This paper presents a numerical investigation to explore the effects of vortex generators on a high speed compressor cascade. Secondary flow effects like the corner separation vort...
Mitigation translocation for conservation of New Zealand skinks
Mitigation translocation for conservation of New Zealand skinks
<p>Worldwide, human development is leading to the expansion and intensification of land use, with increasing encroachment on natural habitats. A rising awareness of the delet...

