في هذا البحث تم اقتراح آلية لجعل المتحكم LQR قادر على قيادة الروبوت
الطائر (Micro Aerial Vehicle by Change Center of Gravity(MAV
COG)) لتعقب مسار محدد , و ملخص هذه التقنية هو إننا قمنا بإضافة مصفوفة تعمل
على توليد المسار الذي نريد تعقبه. و باستخدام برنامج المحاكاة ماتلاب قمنا بتصميم
المتحكم المطلوب.
In our research,
we propose technique to become LQR controller able to drive
(Micro Aerial Vehicle by Change Center of Gravity(MAV COG))
robot on a specific trajectory. We add a matrix to adjust the
trajectory that we want to trace it. We use Matlab program to
execute our controller.
References used
T. Talay,1975- Introduction to the Aerodynamics of Flight . NATIONAL AERONAUTICS AND SPACE ADMINISTRATION ,1,Washignton,204
F.Lesage, N. Hamel, X.Huang, Y.Yuan, M.Khalid and P.Zdunich,2008-Initial Investigation on the Aerodynamic Performance of Flapping wings for Nano Air Vehicles . defence research and development Canada,1,Canada,166
Y. Zhang,2009- Modeling and Hover Control of a Double- Rotor Micro Flying Robot Via Shape Change .Purdue University , 1 , India, 65
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