TY - GEN
T1 - Modeling and simulation analysis of an unmanned tandem ducted fan vehicle with tilting system
AU - Xiang, Changle
AU - Fan, Wei
AU - Liu, Hui
AU - Xu, Bin
AU - Huang, Nan
N1 - Publisher Copyright:
© 2015 IEEE.
PY - 2015/7/7
Y1 - 2015/7/7
N2 - Comprehensive study on control stability analysis before controller design is an indispensable important step for any flight system. In this paper, frequency modal responses and relative input-output controllability are analyzed quantitatively to provide valid instruction for structure improvement. In this project, tilting electric ducted fan (EDF) system is devised for an unmanned tandem ducted fan vehicle to improve the stability and controllability over wind disturbances. Forces and moments of the vehicle are investigated by comprehensive nonlinear modeling. Static thrust experiment has been done for more accurate parameters. Different reference speed of EDFs is considered and studied to evaluate the controllability of different channels.
AB - Comprehensive study on control stability analysis before controller design is an indispensable important step for any flight system. In this paper, frequency modal responses and relative input-output controllability are analyzed quantitatively to provide valid instruction for structure improvement. In this project, tilting electric ducted fan (EDF) system is devised for an unmanned tandem ducted fan vehicle to improve the stability and controllability over wind disturbances. Forces and moments of the vehicle are investigated by comprehensive nonlinear modeling. Static thrust experiment has been done for more accurate parameters. Different reference speed of EDFs is considered and studied to evaluate the controllability of different channels.
UR - http://www.scopus.com/inward/record.url?scp=84941144314&partnerID=8YFLogxK
U2 - 10.1109/ICUAS.2015.7152412
DO - 10.1109/ICUAS.2015.7152412
M3 - Conference contribution
AN - SCOPUS:84941144314
T3 - 2015 International Conference on Unmanned Aircraft Systems, ICUAS 2015
SP - 1196
EP - 1204
BT - 2015 International Conference on Unmanned Aircraft Systems, ICUAS 2015
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2015 International Conference on Unmanned Aircraft Systems, ICUAS 2015
Y2 - 9 June 2015 through 12 June 2015
ER -