تقدم هذه الدراسة تصميماً لمتحكم يعتمد على بنية النموذج المخيخي لرباعية
المحرك.
تمت محاكاة النظام و المتحكم ذو النموذج المخيخي المعتمد على المتحكم PID
باستخدام الحزمة البرمجية ماتلاب ، و تمت مقارنة أداء النظام في ظل وجود ضجيج عند
استخدام المتحكم PID العادي فقط و عند استخدام النموذج المخيخي المعتمد على
المتحكم PID و أظهرت النتائج أن الطريقة الأخيرة تضمن أداء الاستقرار الجيد. كما
تمت مقارنة النظام مع المتحكم ذو النموذج المخيخي المقترح مع نظامين يستخدمان
النموذج المخيخي لهما هيكلية تختلف عن الهيكلية المقترحة.
This paper presents a robust cerebellar model articulation
controller (CMAC) for quadcopter system.
We simulate this systems by using Matlab and Simulink, and we
find that this control guarantees good balance performance and
acceptable robust performance. And we compare our CMAC with
other systems using CMAC but in structures differ of our CMAC
structure.
References used
Domingues, J. (2009): Quadrotor prototype, Universidade Tecnic de Lisboa
Whidborne,J. (2007): Modelling And Linear Control Of A Quadrotor, Cranfield University
Sørensen, A. (2010): Autonomous Control of a Miniature Quadrotor Following Fast Trajectories, Aaloborg University
An ANFIS controller also designed and a comparison
between proposed controller, ANFIS controller and open loop model
had made with different types of disturbance.
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of Method shows the fuzzification value for each prop
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