TY - JOUR
T1 - Aerodynamic parameters from distributed heterogeneous CNT hair sensors with a feedforward neural network
AU - Magar, Kaman Thapa
AU - Reich, Gregory W.
AU - Kondash, Corey
AU - Slinker, Keith
AU - Pankonien, Alexander M.
AU - Baur, Jeffery W.
AU - Smyers, Brian
N1 - Publisher Copyright:
© 2016 IOP Publishing Ltd.
PY - 2016/11/10
Y1 - 2016/11/10
N2 - Distributed arrays of artificial hair sensors have bio-like sensing capabilities to obtain spatial and temporal surface flow information which is an important aspect of an effective fly-by-feel system. The spatiotemporal surface flow measurement enables further exploration of additional flow features such as flow stagnation, separation, and reattachment points. Due to their inherent robustness and fault tolerant capability, distributed arrays of hair sensors are well equipped to assess the aerodynamic and flow states in adverse conditions. In this paper, a local flow measurement from an array of artificial hair sensors in a wind tunnel experiment is used with a feedforward artificial neural network to predict aerodynamic parameters such as lift coefficient, moment coefficient, free-stream velocity, and angle of attack on an airfoil. We find the prediction error within 6% and 10% for lift and moment coefficients. The error for free-stream velocity and angle of attack were within 0.12 mph and 0.37 degrees. Knowledge of these parameters are key to finding the real time forces and moments which paves the way for effective control design to increase flight agility, stability, and maneuverability.
AB - Distributed arrays of artificial hair sensors have bio-like sensing capabilities to obtain spatial and temporal surface flow information which is an important aspect of an effective fly-by-feel system. The spatiotemporal surface flow measurement enables further exploration of additional flow features such as flow stagnation, separation, and reattachment points. Due to their inherent robustness and fault tolerant capability, distributed arrays of hair sensors are well equipped to assess the aerodynamic and flow states in adverse conditions. In this paper, a local flow measurement from an array of artificial hair sensors in a wind tunnel experiment is used with a feedforward artificial neural network to predict aerodynamic parameters such as lift coefficient, moment coefficient, free-stream velocity, and angle of attack on an airfoil. We find the prediction error within 6% and 10% for lift and moment coefficients. The error for free-stream velocity and angle of attack were within 0.12 mph and 0.37 degrees. Knowledge of these parameters are key to finding the real time forces and moments which paves the way for effective control design to increase flight agility, stability, and maneuverability.
KW - aerodynamic parameter prediction
KW - artificial hair sensors
KW - fly by feel
KW - neural network
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U2 - 10.1088/1748-3190/11/6/066006
DO - 10.1088/1748-3190/11/6/066006
M3 - Article
C2 - 27831933
AN - SCOPUS:85011406374
SN - 1748-3182
VL - 11
JO - Bioinspiration and Biomimetics
JF - Bioinspiration and Biomimetics
IS - 6
M1 - 066006
ER -