TY - GEN
T1 - The FWB filter with real-time detector to suppress category II pilot induced oscillation
AU - Yu, Liming
AU - Liu, Hongliang
PY - 2013
Y1 - 2013
N2 - PIO (Pilot Induced Oscillation) is the key factor to damage the flight safety and decrease the quality of manned aircraft. Most of modern PIO records associating with rate limiting or position limiting from actuation systems are defined Category II PIO. The existing compensators, e.g. the Feedback-with-Bypass (FWB) filter, can reduced the oscillation potentiality of the pilot-in-the-loop aircraft system due to rate limiting of control surface, however a negative effect evidently arose which slow the response speed of whole system. This paper uses a Real-Time PIO detector based on Short-time Fourier Transform algorithm as a trigger to determine the switch-off time of the compensator working on the whole system so as to suppress the negative effect on responses of system by FWB. Simulation results show us the positive conclusion that this kind combined FWB filter with Real-Time PIO detector is effectively preventing the Category II PIO without performance decreasing.
AB - PIO (Pilot Induced Oscillation) is the key factor to damage the flight safety and decrease the quality of manned aircraft. Most of modern PIO records associating with rate limiting or position limiting from actuation systems are defined Category II PIO. The existing compensators, e.g. the Feedback-with-Bypass (FWB) filter, can reduced the oscillation potentiality of the pilot-in-the-loop aircraft system due to rate limiting of control surface, however a negative effect evidently arose which slow the response speed of whole system. This paper uses a Real-Time PIO detector based on Short-time Fourier Transform algorithm as a trigger to determine the switch-off time of the compensator working on the whole system so as to suppress the negative effect on responses of system by FWB. Simulation results show us the positive conclusion that this kind combined FWB filter with Real-Time PIO detector is effectively preventing the Category II PIO without performance decreasing.
KW - Actuator rate limiting
KW - Pilot induced oscillation
KW - Real-time detect
UR - https://www.scopus.com/pages/publications/84873183202
U2 - 10.4028/www.scientific.net/AMM.278-280.1713
DO - 10.4028/www.scientific.net/AMM.278-280.1713
M3 - 会议稿件
AN - SCOPUS:84873183202
SN - 9783037855959
T3 - Applied Mechanics and Materials
SP - 1713
EP - 1718
BT - Advances in Mechatronics and Control Engineering
T2 - 2012 International Conference on Mechatronics and Control Engineering, ICMCE 2012
Y2 - 29 November 2012 through 30 November 2012
ER -