Please use this identifier to cite or link to this item:
|Title:||Aircraft-on-ground path following control by dynamical adaptive backstepping|
Nonlinear dynamical systems
|Citation:||Chen, B., Jiao, Z., Ge, S.S. (2013-06). Aircraft-on-ground path following control by dynamical adaptive backstepping. Chinese Journal of Aeronautics 26 (3) : 668-675. ScholarBank@NUS Repository. https://doi.org/10.1016/j.cja.2013.05.003|
|Abstract:||The necessity of improving the air traffic and reducing the aviation emissions drives to investigate automatic steering for aircraft to effectively roll on the ground. This paper addresses the path following control problem of aircraft-on-ground and focuses on the task that the aircraft is required to follow the desired path on the runway by nose wheel automatic steering. The proposed approach is based on dynamical adaptive backstepping so that the system model does not have to be transformed into a canonical triangular form which is necessary in conventional backstepping design. This adaptive controller performs well despite the lack of information on the aerodynamic load and the tire cornering stiffness parameters. Simulation results clearly demonstrate the advantages and effectiveness of the proposed approach. © 2013 Production and hosting by Elsevier Ltd. on behalf of CSAA & BUAA.|
|Source Title:||Chinese Journal of Aeronautics|
|Appears in Collections:||Staff Publications|
Show full item record
Files in This Item:
There are no files associated with this item.
checked on Oct 11, 2018
WEB OF SCIENCETM
checked on Oct 2, 2018
checked on May 11, 2018
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.