کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
755303 1462519 2013 8 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Aircraft-on-ground path following control by dynamical adaptive backstepping
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مهندسی هوافضا
پیش نمایش صفحه اول مقاله
Aircraft-on-ground path following control by dynamical adaptive backstepping
چکیده انگلیسی

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.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Chinese Journal of Aeronautics - Volume 26, Issue 3, June 2013, Pages 668–675
نویسندگان
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