نشریه مهندسی مکانیک ایران

نشریه مهندسی مکانیک ایران

طراحی قانون هدایت برای فاز نهایی ماموریت فرود سه بعدی بوستر با روش بسط مرتبه بالا

نوع مقاله : مقاله علمی پژوهشی

نویسندگان
1 دکتری، دانشگاه صنعتی مالک اشتر، مجتمع دانشگاهی برق و کامپیوتر، ایران
2 دانشیار، دانشگاه صنعتی مالک اشتر، مجتمع دانشگاهی برق و کامپیوتر، ایران
3 استادیار، دانشگاه صنعتی مالک اشتر، مجتمع دانشگاهی برق و کامپیوتر، ایران
چکیده
در این مقاله، طراحی قانون هدایت بهینه با در نظر گرفتن شرایط و زمان نهایی مقید برای مرحله نهایی مسئله فرود سه بعدی بوستر یک ماهواره بر مورد بررسی قرار گرفته است. هدف اصلی تحقیق، بررسی نحوه توسعه و افزایش قابلیت روش بسط مرتبه بالای برداری برای طراحی قانون هدایت بهینه است. این قانون نسبت به انحرافات بزرگ اولیة متغیر حالت، حساسیت حداقلی دارد و همچنین امکان پیاده سازی آنلاین آن با حداقل محاسبات در عمل وجود دارد. اثر بخشی روش بسط مرتبه بالا با شبیه سازی مونت کارلو مورد بررسی قرار گرفته است و نشان ‌داده‌ شد که قانون هدایت بر اساس بسط مرتبه بالای برداری نه تنها از دقت مناسبی برخوردار است بلکه می تواند جایگزین خوبی برای مسئله تعقیب مسیر نامی باشد.
کلیدواژه‌ها

موضوعات


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  • تاریخ دریافت 16 آذر 1401
  • تاریخ بازنگری 23 تیر 1402
  • تاریخ پذیرش 15 مهر 1402