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طراحی کنترل گر رهگیر جهت شبیه سازی حین پرواز رفتار هواپیمای جت جنگنده توسط جت بدون سرنشین | ||
مهندسی مکانیک دانشگاه تبریز | ||
مقاله 25، دوره 47، شماره 3، آذر 1396، صفحه 225-234 اصل مقاله (1.23 M) | ||
نوع مقاله: مقاله پژوهشی | ||
نویسندگان | ||
سید جواد محمدی بایگی* 1؛ مهدی مرتضوی2 | ||
1دانشگاه آزاد اسلامی واحد دامغان | ||
2دانشیار، دانشکده مهندسی، دانشگاه اصفهان، اصفهان، ایران | ||
چکیده | ||
در این مقاله امکان شبیهسازی حین پرواز رفتار دینامیک طولی و عرضی یک هواپیمای جت جنگنده توسط یک جت بدون سرنشین مورد ارزیابی قرار گرفته و کنترلگر مورد نیاز برای اجرای شبیه سازی حین پرواز و رهگیری مسیر پروازی آن طراحی شده است. طراحی کنترلگر بر اساس روش جایدهی قطب و رهگیری مسیر به انجام رسیده و در آن کنترلگر به نحوی طراحی شده است که جت بدون سرنشین قادر به تعقیب رفتار دینامیک طولی و عرضی هواپیمای جت جنگنده در حین پرواز باشد. در این راستا پس از به کارگیری کنترلگر طراحی شده در جت بدون سرنشین به شبیه سازی رفتار جت جنگنده توسط آن پرداخته و نتایج شبیهسازی حاکی از رهگیری مطلوب رفتار دینامیکی هواپیمای جت جنگنده توسط جت بدون سرنشین در محدوده مشترک عملکردی آنها میباشد. برای صحه گذاری بر طراحی انجام شده به شبیه سازی اطلاعات تست پروازی جتجنگنده توسط جت بدون سرنشین پرداخته شده است. مقایسه نتایج شبیه سازی با اطلاعات تست پروازی جت جنگنده، توانایی شبیه سازی حین پرواز رفتار دینامیکی جت جنگنده توسط جت بدون سرنشین را به اثبات میرساند. | ||
کلیدواژهها | ||
مدل مشابه دینامیکی؛ شبیه سازی حین پرواز؛ جایدهی قطب؛ داده های تست پرواز | ||
مراجع | ||
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