دوره 14، شماره 1 - ( مجله کنترل، جلد 14، شماره 1، بهار 1399 )                   جلد 14 شماره 1,1399 صفحات 49-63 | برگشت به فهرست نسخه ها

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Rajabi M J, Vali A R, Behnamgol V. Design of integrated Guidance and control system in the pitch channel using observer based chattering free sliding mode theory. JoC. 2020; 14 (1) :49-63
URL: http://joc.kntu.ac.ir/article-1-577-fa.html
رجبی محمدجواد، ولی احمد رضا، بهنام گل وحید. طراحی سیستم هدایت و کنترل یکپارچه در کانال فراز با استفاده از تئوری مد لغزشی هموار مبتنی بر رؤیت گر. مجله کنترل. 1399; 14 (1) :49-63

URL: http://joc.kntu.ac.ir/article-1-577-fa.html


1- دانشگاه صنعتی مالک اشتر
چکیده:   (1967 مشاهده)
طراحی سیستم هدایت و کنترل یکپارچه در اجسام پرنده یکی از زمینه‌های تحقیقاتی در حوزه هوافضا بوده که در سال‌های اخیر موردتوجه محققین قرارگرفته است. به دلیل غیرخطی بودن معادلات سینماتیکی و دینامیکی رهگیرهای آشیانه یاب در فاز نهایی و وجود نامعینی‌هایی ازجمله مانورهای هدف، اغتشاشات خارجی و تغییرات ضرایب آیرودینامیک، تئوری کنترل مد لغزشی یک روش مناسب برای طراحی سیستم هدایت و کنترل یکپارچه است. بزرگ‌ترین مشکل روش مد لغزشی، وجود نوسانات فرکانس بالا در سیگنال کنترل است که پیاده‌سازی این کنترل‌کننده را غیرممکن می‌سازد. یک روش برای هموارسازی سیگنال کنترل در روش مد لغزشی، استفاده از رؤیت گر است. در این مقاله با در اختیار داشتن تخمین اغتشاش و با استفاده از ساختاری متفاوت نسبت به روش مد لغزشی استاندارد، سیگنال کنترل کاملاً هموارشده است. همچنین همگرایی زمان محدود در حضور نامعینی تضمین‌شده است. سیستم هدایت و کنترل طراحی‌شده با استفاده از روش پیشنهادی در شبیه‌سازی کامپیوتری مورد ارزیابی قرارگرفته است.
متن کامل [PDF 794 kb]   (147 دریافت)    
نوع مطالعه: پژوهشي | موضوع مقاله: تخصصي
دریافت: 1397/2/6 | پذیرش: 1397/5/21 | انتشار: 1399/3/22

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