نوع مقاله : علمی پژوهشی

نویسندگان

1 دانشجوی دکتری، دانشکده مهندسی مکانیک، دانشگاه صنعتی خواجه نصیرالدین طوسی، تهران

2 استادیار، دانشکده مهندسی مکانیک، دانشگاه صنعتی خواجه نصیرالدین طوسی، تهران

10.22034/jtae.2024.8.2.3

چکیده

این مقاله به تشریح روند طراحی و شبیه‌‌سازی عملکرد کنترل‌‌کننده‌‌ پیش بین مدل بهینه می‌‌پردازد که به منظور هدایت موشک در یک مساله دو بعدی کمینه‌‌سازی زمان برخورد و فاصله از دست دهی با هدف ایجاد شده‌‌اند. در طراحی کنترل‌‌کننده پیش بین 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 گرفته‌‌ است. با توجه به شبیه‌سازی ها می‌‌توان نشان داد که کنترل‌‌کننده پیش‌‌بین مدل خطی ضمنی (برخط) و کنترل کننده پیش‌بین مدل غیرخطی بهینه، فاصله برخورد نهایی موشک با هدف و زمان برخورد را به خوبی کنترل می‌کند. نوآوری این مقاله طراحی کنترل کننده پیش‌بین مدل بهینه با استفاده 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 a homing missile using optimal linear and nonlinear model predictive control

نویسندگان [English]

  • mohamad mahdi soori 1
  • seyed hosein Sadati 2

1 PhD 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 (on-line) and the predictive controller of the optimal non-linear 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 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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