TY - JOUR
T1 - Prediction of nonlinear pilot-induced oscillation using an intelligent human pilot model
AU - XU, Shuting
AU - TAN, Wenqian
AU - QU, Xiangju
AU - ZHANG, Cheng
N1 - Publisher Copyright:
© 2019 Chinese Society of Aeronautics and Astronautics
PY - 2019/12
Y1 - 2019/12
N2 - This paper proposes a method to predict nonlinear Pilot-Induced Oscillation (PIO) using an intelligent human pilot model. This method is based on a scalogram-based PIO metric, which uses wavelet transforms to analyze the nonlinear characteristics of a time-varying system. The intelligent human pilot model includes three modules: perception module, decision and adaptive module, and execution module. Intelligent and adaptive features, including a neural network receptor, fuzzy decision and adaptation, are also introduced into the human pilot model to describe the behavior of the human pilot accommodating the nonlinear events. Furthermore, an algorithm is proposed to describe the procedure of the PIO prediction method with nonlinear evaluation cases. The prediction results obtained by numerical simulation are compared with the assessments of flight test data to validate the utility of the method. The flight test data were generated in the evaluation of the Smart-Cue/Smart-Gain, which is capable of reducing the PIO tendencies considerably. The results show that the method can be applied to predict the nonlinear PIO events by human pilot model simulation.
AB - This paper proposes a method to predict nonlinear Pilot-Induced Oscillation (PIO) using an intelligent human pilot model. This method is based on a scalogram-based PIO metric, which uses wavelet transforms to analyze the nonlinear characteristics of a time-varying system. The intelligent human pilot model includes three modules: perception module, decision and adaptive module, and execution module. Intelligent and adaptive features, including a neural network receptor, fuzzy decision and adaptation, are also introduced into the human pilot model to describe the behavior of the human pilot accommodating the nonlinear events. Furthermore, an algorithm is proposed to describe the procedure of the PIO prediction method with nonlinear evaluation cases. The prediction results obtained by numerical simulation are compared with the assessments of flight test data to validate the utility of the method. The flight test data were generated in the evaluation of the Smart-Cue/Smart-Gain, which is capable of reducing the PIO tendencies considerably. The results show that the method can be applied to predict the nonlinear PIO events by human pilot model simulation.
KW - Flight simulation
KW - Human pilot model
KW - Human-vehicle system
KW - Nonlinear system
KW - Pilot-induced oscillation
UR - https://www.scopus.com/pages/publications/85075534186
U2 - 10.1016/j.cja.2019.06.003
DO - 10.1016/j.cja.2019.06.003
M3 - 文章
AN - SCOPUS:85075534186
SN - 1000-9361
VL - 32
SP - 2592
EP - 2611
JO - Chinese Journal of Aeronautics
JF - Chinese Journal of Aeronautics
IS - 12
ER -