فناوری در مهندسی هوافضا

فناوری در مهندسی هوافضا

هدایت و کنترل یکپارچه کانال اوج موشک آشیانه‌یاب با‌استفاده از کنترل پیش‌بین مدل خطی و غیرخطی بهینه

نوع مقاله : علمی پژوهشی

نویسندگان
1 دانشجوی دکتری، دانشکده مهندسی مکانیک، دانشگاه صنعتی خواجه نصیرالدین طوسی، تهران
2 دانشیار، دانشکده مهندسی مکانیک، دانشگاه صنعتی خواجه نصیرالدین طوسی، تهران
چکیده
این مقاله به تشریح روند طراحی و شبیه‌‌سازی عملکرد کنترل‌‌کننده‌‌ پیش‌بین مدل بهینه می‌‌پردازد که به‌منظور هدایت موشک در یک مسئله دوبعدی کمینه‌‌سازی زمان برخورد و فاصله از دست دهی با هدف ایجاد شده‌‌اند. در طراحی کنترل‌‌کننده پیش‌بین مدل بهینه، ابتدا نوع پرکاربرد مدل پیش‌‌بین خطی ضمنی طراحی شده و سپس مدل پیش‌‌بین غیرخطی ارائه شده و عملکرد آن‌‌ها در هدایت موشک مورد ارزیابی قرار ‌‌گرفته‌است. باتوجه به شبیه‌سازی‌‌ها می‌‌توان نشان داد که کنترل‌‌کننده پیش‌‌بین مدل خطی ضمنی (برخط) و کنترل‌کننده پیش‌بین مدل غیرخطی بهینه، فاصله برخورد نهایی موشک با هدف و زمان برخورد را به خوبی کنترل می‌کند. نوآوری این مقاله  طراحی کنترل‌کننده پیش‌بین مدل بهینه با‌استفاده از الگوریتم ژنتیک و اجتماع ذرات در مدل هدایت و کنترل یکپارچه است.
کلیدواژه‌ها
موضوعات

عنوان مقاله English

Integrated Guidance and Control of the Pitch Channel in Homing Missile Using Optimal Linear and Nonlinear Model Predictive Control

نویسندگان English

Mohammad Mahdi Soori 1
Seyed Hosein Sadati 2
1 Ph. D.Student, Mechanical Engineering Department, K. N. Toosi University of Technology, Tehran
2 Assistant Professor, Mechanical Engineering Department, K. N. Toosi University of Technology, Tehran
چکیده English

This article describes the process of designing and simulating the performance of the predictive controller of the optimal model, which was created in order to guide the missile in a two-dimensional problem of minimizing the collision time and the distance from the target. In the design of the optimal model predictive controller, first, the widely used type of implicit linear predictive model is designed, and then the nonlinear predictive model is presented, and their performance in missile guidance is evaluated. According to the simulations, it can be shown that the predictive controller of the implicit linear model (online) and the predictive controller of the optimal nonlinear model control the distance of the missile's final collision with the target and the collision time well. The innovation of this article is the design of the predictive controller of the optimal model using a genetic algorithm and particle community in the integrated guidance and control model.

کلیدواژه‌ها English

Missile
Optimal Control
Model Predictive Control
Integrated Guidance and Control
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  • تاریخ دریافت 04 دی 1401
  • تاریخ بازنگری 15 مرداد 1402
  • تاریخ پذیرش 18 مرداد 1402
  • تاریخ اولین انتشار 18 مرداد 1402