Aircraft-on-ground path following control by dynamical adaptive backstepping  

作　　者：Chen Bihua Jiao Zongxia Shuzhi Sam Ge 

机构地区：[1]Science and Technology on Aircraft Control Laboratory, Beihang University [2]Department of Electrical & Computer Engineering, National University of Singapore

出　　处：《Chinese Journal of Aeronautics》2013年第3期668-675,共8页中国航空学报（英文版）

基　　金：the National Nature Science Foundation for Distinguished Young Scholars of China(Grant No.50825502)

摘　　要：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.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.

关 键 词：Adaptive control Aircraft-on-ground BACKSTEPPING Nonlinear dynamical systems Path following 

分 类 号：V249.1[航空宇航科学与技术—飞行器设计]