TY - GEN
T1 - Machine learning for flapping wing flight control
AU - Goedhart, Menno W.
AU - Van Kampeny, Erik Jan
AU - Armaniniz, Sophie F.
AU - De Visser, Coen C.
AU - Chu, Qiping
N1 - Publisher Copyright:
© 2018 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
PY - 2018/1/1
Y1 - 2018/1/1
N2 - Flight control of Flapping Wing Micro Air Vehicles is challenging, because of their complex dynamics and variability due to manufacturing inconsistencies. Machine Learning algorithms can be used to tackle these challenges. A Policy Gradient algorithm is used to tune the gains of a Proportional-Integral controller using Reinforcement Learning. A novel Classification Algorithm for Machine Learning control (CAML) is presented, which uses model identification and a neural network classifier to select from several predefined gain sets. The algorithms show comparable performance when considering variability only, but the Policy Gradient algorithm is more robust to noise, disturbances, nonlinearities and apping motion. CAML seems to be promising for problems where no single gain set is available to stabilize the entire set of variable systems.
AB - Flight control of Flapping Wing Micro Air Vehicles is challenging, because of their complex dynamics and variability due to manufacturing inconsistencies. Machine Learning algorithms can be used to tackle these challenges. A Policy Gradient algorithm is used to tune the gains of a Proportional-Integral controller using Reinforcement Learning. A novel Classification Algorithm for Machine Learning control (CAML) is presented, which uses model identification and a neural network classifier to select from several predefined gain sets. The algorithms show comparable performance when considering variability only, but the Policy Gradient algorithm is more robust to noise, disturbances, nonlinearities and apping motion. CAML seems to be promising for problems where no single gain set is available to stabilize the entire set of variable systems.
UR - https://www.scopus.com/pages/publications/85141587532
U2 - 10.2514/6.2018-2135
DO - 10.2514/6.2018-2135
M3 - Conference contribution
AN - SCOPUS:85141587532
SN - 9781624105272
T3 - AIAA Information Systems-AIAA Infotech at Aerospace, 2018
BT - AIAA Information Systems-AIAA Infotech at Aerospace
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Information Systems-AIAA Infotech at Aerospace, 2018
Y2 - 8 January 2018 through 12 January 2018
ER -