كيفية الاقتباس
تواريخ المنشور
الإستلام
النسخة النهائية
الموافقة
النشر الالكتروني
الملخص
تقدم هذه الورقة خوارزمية تحكم جديدة مثالية ومتينة قائمة على متحكم التكامل النسبي (PI) ووحدة التحكم في رد الفعل الراجع (SFB) مع مراقب اضطراب الحالة لنظام طائرات هليكوبتر تتحرك بدرجتين من الحرية. بدلا من استخدام الكسب العالي لرفض الاضطراب الخارجي، تم استخدام مراقب الاضطراب لتحسين متانة وحدة التحكم المقترحة. في حين تم تحسين أداء النظام المتحكم به من خلال الجمع بين وحدة التحكم PI ووحدة التحكم في ردود الفعل الخاصة بالحالة. من أجل التحقق من أداء ومتانة طريقة التحكم المقترحة، تم اجراء عمليات محاكاة تعتمد على Matlab 2022 لمقارنة وحدة التحكم المقترحة مع وحدة التحكم LQR. تمت المقارنة بين المتحكمات في ثلاث حالات: 1) النموذج الاسمي 2) رفض الاضطراب 3) عدم يقين النظام. تظهر الخوارزمية المقترحة خصائص جيدة بالقرب من تردد القطع، والتي يمكن تأكيدها بوضوح من خلال نتائج المجال الزمني.
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