کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
720253 892291 2007 6 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
ADAPTIVE FUZZY BACKLASH COMPENSATION FOR A NEW DYNAMIC FLIGHT SIMULATOR
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مکانیک محاسباتی
پیش نمایش صفحه اول مقاله
ADAPTIVE FUZZY BACKLASH COMPENSATION FOR A NEW DYNAMIC FLIGHT SIMULATOR
چکیده انگلیسی

In this paper we addressed the problem of improving the control of DC motors used for the specific application of 3 degrees of freedom moving base flight simulator. Indeed the presence of backlash in DC motors gearboxes induces shocks and naturally limits the flight feeling. In this paper, dynamic inversion with Fuzzy Logic is used to design an adaptive backlash compensator. The classification property of fuzzy logic techniques makes them a natural candidate for the rejection of errors induced by the backlash. A tuning algorithm is given for the fuzzy logic parameters, so that the output backlash compensation scheme becomes adaptive. The fuzzy backlash compensator is first validated using a realistic model of the mechanical system and is actually tested on the real flight simulator.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: IFAC Proceedings Volumes - Volume 40, Issue 21, 2007, Pages 151-156