Please use this identifier to cite or link to this item: https://doi.org/10.1109/ICCA.2010.5524138
Title: Flight control design with hierarchical dynamic inversion
Authors: Peng, K. 
Lum, K.Y. 
Chen, B.M. 
Keywords: Dynamic inversion
Flight control
Flight control system
Nonlinear system control method
Unmanned aerial vehicle
Issue Date: 2010
Source: Peng, K.,Lum, K.Y.,Chen, B.M. (2010). Flight control design with hierarchical dynamic inversion. 2010 8th IEEE International Conference on Control and Automation, ICCA 2010 : 297-302. ScholarBank@NUS Repository. https://doi.org/10.1109/ICCA.2010.5524138
Abstract: Hierarchical dynamic inversion (HDI) is proposed together with newly developed variant-factor and recursive control techniques to design autonomous flight control (AFC) laws for fixed-wing aircraft. HDI is applicable to control design of some non-affine nonlinear systems to which dynamic inversion is not applicable. The AFC law designed with HDI at the nominal flight condition is applicable to other flight conditions in a wide flight envelope so that workload can be reduced significantly in AFC design compared to gain scheduling. The simulation results demonstrate that with the AFC law designed with HDI, the aircraft successfully completes the pre-scheduled maneuvering flight in a subsonic flight envelope. © 2010 IEEE.
Source Title: 2010 8th IEEE International Conference on Control and Automation, ICCA 2010
URI: http://scholarbank.nus.edu.sg/handle/10635/70345
ISBN: 9781424451951
DOI: 10.1109/ICCA.2010.5524138
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