علوم، فناوری و کاربردهای فضایی

علوم، فناوری و کاربردهای فضایی

مدل‌سازی، شبیه‏‌سازی و آنالیز دینامیک ماهواره انعطاف‌‏پذیر در MATLAB و ADAMS و صحت‌سنجی طراحی به منظور کاربردهای کنترل وضعیت

نوع مقاله : مقاله پژوهشی

نویسنده
دانشگاه صنعتی خواجه نصیرالدین طوسی
چکیده
امروزه به منظور تأمین توان الکتریکی از آرایه‌های خورشیدی انعطاف‌پذیر در بسیاری از ماهواره‌ها استفاده می‌شود. با وجود این طراحی قانون کنترل وضعیت برای یک ماهواره با اجزاء انعطاف‌پذیر بزرگ شامل دشواری‌هایی از جمله مدل‌سازی و دینامیک پیچیده می‌باشد. در این مقاله، انواع روش‌های مدل‌سازی ماهواره‌ی انعطاف‌پذیر بررسی شده و روش المان محدود جهت آنالیز مودال پیشنهاد می‌شود. در ادامه آنالیز مودهای فرکانسی ماهواره‌ی انعطاف‌پذیر به‌عنوان یک تیر یکسر گیردار متصل به بدنه صلب شامل مدل تحلیلی پیاده‌سازی شده در MATLAB و شبیه‌سازی المان محدود‏ ارائه می‌شود. بدین منظور از ADAMS، Patran/Nastran و Abaqus جهت مدل‌سازی بهره‌گیری می‌شود که مشخصات فیزیکی ماهواره انعطاف‌پذیر با استفاده از پارامترهای Intelsat-5 تعیین می‌شود. مقایسه عملکرد روش‌های آنالیز مودال با مدل عملیاتی ماهواره، حداکثر خطای نسبی 3.34 درصد را نشان می‌دهد. این تفاوت حاصل از مش‌بندی‌های متفاوت جهت آنالیز مودال، در نرم‌افزارهای شبیه‌سازی می‌باشد. در انتها صحت‌سنجی مدل با استفاده از شبیه‌سازی چندموضوعی ماهواره انعطاف‌پذیر صورت گرفته که خطای نسبی بین شبیه‌سازی‌های MATLAB و ADAMS قابل قبول می‌باشد. نتایج بیانگر کارآیی مدل‌های المان محدود جهت مدل‌سازی و حل معادلات دینامیک ماهواره‌ی انعطاف‌پذیر بوده که می‌تواند برای هدف طراحی قانون کنترل وضعیت مورد استفاده قرار گیرد.
کلیدواژه‌ها
موضوعات

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دوره 6، شماره 1
مهر 1405
صفحه 132-149

  • تاریخ دریافت 18 شهریور 1404
  • تاریخ بازنگری 08 آبان 1404
  • تاریخ پذیرش 18 خرداد 1405