TY - GEN
T1 - Adaptive feedforward control design for gust loads alleviation and LCO suppression
AU - Wang, Y.
AU - Da Ronch, A.
AU - Ghandchi-Therani, M.
AU - Li, F.
N1 - Copyright:
Copyright 2014 Elsevier B.V., All rights reserved.
PY - 2014
Y1 - 2014
N2 - An adaptive feedforward controller is designed for gust loads alleviation and limit cycle oscillations suppression. Two sets of basis functions, based on the finite impulse response and modified finite impulse response approaches, are investigated to design the controller for gust loads alleviation. Limit cycle oscillations suppression is shown by using the modified finite impulse response controller. Worst case gust search is performed by using a nonlinear technique of model reduction to speed up the costs of calculations. Both the "one-minus-cosine" and Von Kármán continuous turbulence gusts of different intensities were generated to examine the performance of controllers. The responses of these two types of gust can be reduced effectively by finite impulse response controller in the whole process, while the modified finite impulse response controller is found to increase the loads during the initial transient response. The above two types of gust induced limit cycle oscillations were used to test the modified finite impulse response controller. Results show that it can suppress limit cycle oscillations to some extent.
AB - An adaptive feedforward controller is designed for gust loads alleviation and limit cycle oscillations suppression. Two sets of basis functions, based on the finite impulse response and modified finite impulse response approaches, are investigated to design the controller for gust loads alleviation. Limit cycle oscillations suppression is shown by using the modified finite impulse response controller. Worst case gust search is performed by using a nonlinear technique of model reduction to speed up the costs of calculations. Both the "one-minus-cosine" and Von Kármán continuous turbulence gusts of different intensities were generated to examine the performance of controllers. The responses of these two types of gust can be reduced effectively by finite impulse response controller in the whole process, while the modified finite impulse response controller is found to increase the loads during the initial transient response. The above two types of gust induced limit cycle oscillations were used to test the modified finite impulse response controller. Results show that it can suppress limit cycle oscillations to some extent.
KW - Adaptive feedforward control
KW - Aeroelastic model
KW - Gust loads alleviation
KW - LCO suppression
UR - https://www.scopus.com/pages/publications/84910647320
M3 - Conference contribution
AN - SCOPUS:84910647320
T3 - 29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014
BT - 29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014
PB - International Council of the Aeronautical Sciences
T2 - 29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014
Y2 - 7 September 2014 through 12 September 2014
ER -