مقایسة چارچوب‌های بهینه‌سازی چندموضوعی در طراحی حامل‌ فضایی

نوع مقاله : مقاله پژوهشی

نویسنده

عضو هیات علمی / پژوهشگاه هوافضا، وزارت علوم، تحقیقات و فناوری

چکیده

در این مقاله، ضمن معرفی چارچوب‌های جدید طراحی بهینة چندموضوعی حامل‌های فضایی، کارآیی چارچوب‌های بهینة چندموضوعی نیز بررسی شده است. طی سالیان اخیر، دو چارچوب اصلی طراحی بهینة چندموضوعی به‌کار رفته در طراحی حامل‌های فضایی، طراحی بهینة چندموضوعی و طراحی همزمان جامع بوده است. مورد نخست براساس روش‌های بهینه‌سازی در قالب روش‌های بهینه‌سازی چندموضوعی، امکان طراحی چندموضوعی توسعه یافته و مورد دوم با بهره‌گیری از منطق فازی و تبدیل مسئلة بهینه‌سازی چندهدفی مقید به بهینه‌سازی تک‌هدفی نامقید توسعه یافته است. در این مقاله دو چارچوب مورد اشاره برای طراحی بهینة چندموضوعی حامل‌های فضایی پیاده‌سازی شده است. برای ارزیابی کارآیی چارچوب‌های طراحی از منظر زمان اجرا و دقت نتایج، از نتایج حاصل از پیاده‌سازی دو چارچوب برای یک حامل فضایی موجود استفاده شده است. نتایج حاکی از دقت بالاتر چارچوب طراحی بهینة چندموضوعی و زمان اجرای کمتر چارچوب طراحی همزمان جامع است. گفتنی است چارچوب طراحی بهینة چندموضوعی در مجامع علمی توسعة چشمگیری یافته است، این در حالی است که طراحی همزمان جامع در ابتدای راه توسعة بهینه‌سازی چندموضوعی قرار دارد.

کلیدواژه‌ها

موضوعات

عنوان مقاله [English]

Comparing the launch vehicle multidisciplinary design optimization frameworks

نویسنده [English]

  • Hassan Naseh
چکیده [English]

The main aim of this paper is introducing the launch vehicle multidisciplinary design optimization frameworks and also considering the performance of them (aspects of processing time and accuracy). Recently, two multidisciplinary design optimization frameworks are applied for optimizing launch vehicles are Multidisciplinary Design Optimization (MDO) and Holistic Concurrent Design (HCD). The first framework is developed based on Multidisciplinary Design Feasible (MDF) and the second one is established the fuzzy rule set based on designer's expert knowledge with a holistic approach. For assessment of performance the frameworks from time and accuracy aspects utilized the result of applying the frameworks on existing launch. The achieved results have shown the more accuracy in MDO and less processing time in HCD frameworks. That is noticed the MDO framework is developed in scientific literature and the HCD framework has not developed yet. Finally, the MDO and HCD methodologies are recommended to apply the multidisciplinary problems.

کلیدواژه‌ها [English]

  • optimal design
  • multidisciplinary
  • launch vehicle
  • MDO
  • HCD

مراجع

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