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

آدمی, امیرحسین; طائی, حجت; حضوری, منصور

doi:10.30699/jsst.2019.1123

نوع مقاله : مقالة‌ تحقیقی‌ (پژوهشی‌)

نویسندگان

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

² عضو هیئت علمی مجتمع دانشگاهی هوافضا، دانشگاه صنعتی مالک اشتر، تهران، ایران

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

https://doi.org/10.30699/jsst.2019.1123

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

20.1001.1.20084560.1398.12.1.4.7

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.Tehran.IRAN

² Faculty member of Aerospace University Complex, Malek Ashtar University of Technology, Tehran, IRAN

³ Department of Aerospace Engineering, Malek Ashtar University of Technology, Tehran, IRAN

چکیده [English]

Considering the importance of the presence of uncertainties in the design of complex engineering systems, in this research multidisciplinary design optimization process for a bipropellant propulsion system in the presence of uncertainties, which in addition to minimizing the system mass, has a high robust. Based on this, the multidisciplinary design view of the bipropellant propulsion system is expressed in both optimum design and optimum robust design. The continued with the application of uncertainties, the mass, operational and geometric results of the propulsion system are expressed in terms of optimum design, robust design and optimum robust design. According to the results, it is shown that the lowest mass occurs in optimum design mode. But with uncertainties, it is observed at this point that it has the least robust and reliability. It also attempts to explain the difference between the concepts of robust design and optimum design with the help of results

کلیدواژه‌ها [English]

Multidisciplinary design optimization
Bipropellant propulsion system
Uncertainty
Robust design optimization

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علوم و فناوری فضایی

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

مراجع

مراجع

دوره 12، شماره 1 - شماره پیاپی 38
فروردین 1398
صفحه 41-53

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

مراجع

مراجع

دوره 12، شماره 1 - شماره پیاپی 38فروردین 1398صفحه 41-53

دوره 12، شماره 1 - شماره پیاپی 38
فروردین 1398
صفحه 41-53