Please use this identifier to cite or link to this item: https://doi.org/10.1016/j.cja.2013.05.003
Title: Aircraft-on-ground path following control by dynamical adaptive backstepping
Authors: Chen, B.
Jiao, Z.
Ge, S.S. 
Keywords: Adaptive control
Aircraft-on-ground
Backstepping
Nonlinear dynamical systems
Path following
Issue Date: Jun-2013
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
URI: http://scholarbank.nus.edu.sg/handle/10635/81941
ISSN: 10009361
DOI: 10.1016/j.cja.2013.05.003
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