ارزیابی سه روش طراحی بهینه، مقاوم و بهینه مقاوم چندموضوعی سامانه پیشرانش دومولفه ای

نویسندگان

1 مدیر مرکز ماهواره و فضاپیما، مجتمع دانشگاهی هوافضا، دانشگاه صنعتی مالک اشتر

2 عضو هیات علمی/دانشگاه صنعتی مالک اشتر

3 مجتمع دانشگاهی هوافضا،دانشگاه صنعتی مالک اشتر،تهران،ایران

چکیده

 با توجه به اهمیت حضور عدم قطعیت­ ها در طراحی سیستم ­های پیچیده مهندسی، در این پژوهش، روند طراحی بهینه چندموضوعی سیستم پیشرانش دومولفه­ای در حضور عدم قطعیت­ ها ارائه می­گردد که علاوه بر کمینه نمودن جرم سیستم از مقاومت مطلوبی نسبت به عدم ­قطعیت­ ها برخوردار باشد. براین اساس روندنمای طراحی چندموضوعی سیستم پیشرانش دومولفه ­ای در دو حالت طراحی بهینه و طراحی بهینه مقاوم نشان ­داده می­شود. سپس با اعمال عدم قطعیت­ ها، نتایج جرمی، عملکردی و هندسی سیستم پیشرانش به تفکیک برای طراحی بهینه، طراحی مقاوم و طراحی بهینه مقاوم بیان می­گردد. با توجه به نتایج نشان داده می­شود که کمترین جرم در حالت طراحی بهینه اتفاق می­افتد. اما با اعمال عدم قطعیت­ ها در این­ نقطه مشاهده می­ گردد که کمترین مقاومت و قابلیت اطمینان را دارا می­ باشد. همچنین سعی می­شود تفاوت مفاهیم طراحی مقاوم و طراحی بهینه مقاوم به کمک نتایج تشریح ­شود.

کلیدواژه‌ها


عنوان مقاله [English]

Evaluation of Three Design approach of a bipropellant propulsion system including multidisciplinary design optimization, Robust and Optimum-Robust

نویسندگان [English]

  • Amirhossain Adami 1
  • Hojat Taei 2
  • Mansour Hozuri 3
1 Satellite & LV center, Aerospace Department, Malek Ashtar University of Technology
2 Malek Ashtar University
3 Department of Aerospace Engineering, Malek Ashtar University of Technology, Tehran, Iran.

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