طراحی کنترل‌کننده مود لغزشی با پارامترهای بهینه برای هدایت سه‌بعدی موشک با استفاده از الگوریتم جستجوی هارمونی

نوع مقاله : گرایش دینامیک، ارتعاشات و کنترل

نویسندگان

1 گروه مهندسی برق-کنترل، دانشکده فنی و مهندسی، دانشگاه بین المللی امام خمینی، قزوین، ایران

2 گروه مهندسی مکانیک، دانشکده فنی و مهندسی، دانشگاه بین المللی امام خمینی، قزوین، ایران

چکیده

در این مقاله به طراحی قانون هدایت ناوبری مبتنی بر کنترل مود لغزشی با استفاده از الگوریتم جستجوی هارمونی برای ردیابی هدف دارای مانور در فضای سه­بعدی پرداخته شده است. علی­رغم کارایی بالای قوانین هدایت کلاسیک در ردیابی هدف بدون مانور، برای مواردی که نامعینی و اغتشاش، غیرخطی بودن فرایند دینامیکی و مانور هدف وجود داشت، نیاز به قانون هدایت ناوبری مقاوم احساس گردید. از همین رو از روش کنترل مود لغزشی به­عنوان کنترل­کننده­ای مقاوم برای طراحی قانون هدایت موشک در فضای سه­بعدی استفاده شده است. با کمینه­سازی تابع برازش چند هدفه مجموع وزنی فاصله نسبی میان موشک و هدف و زاویه یاو خط دید توسط الگوریتم جستجوی هارمونی، پارامترهای مود لغزشی به­طور بهینه تعیین شده­اند. به­منظور نشان دادن کارایی و توانایی روش پیشنهادی، نتایج به­دست­آمده با برخی    روش­های هدایت و ناوبری از قبیل هدایت ناوبری تناسبی (PNG) و هدایت ناوبری تناسبی الحاقی (APNG) مقایسه شده است. نتایج        به­دست­آمده نشان­دهنده بهبود عملکرد و کارایی قانون هدایت مبتنی­بر مود لغزشی تنظیم شده نسبت به این روش­های طراحی قانون هدایت می­باشد.

کلیدواژه‌ها

عنوان مقاله [English]

Design of a Sliding Mode Controller with Optimal Parameters for Three-Dimensional Guidance Law Using Harmony Search Algorithm

نویسندگان [English]

  • Hasan Nasiri Soloklo 1
  • Amir Farhad Ehyaei 1
  • Javad Ehyaei 2
1 Electrical Engineering Department, Faculty of Technical and Engineering, Imam Khomeini International University, Qazvin, Iran
2 Mechanical Engineering Department, Faculty of Technical and Engineering, Imam Khomeini International University, Qazvin, Iran
چکیده [English]

In this paper, a navigation guidance law is designed based on a sliding mode control and harmony search algorithm to track a maneuvering target in three-dimensional space. Despite the high efficiency of classical guidance laws in target tracking without any maneuvering, in the presence of uncertainty, disturbance, the nonlinearity of dynamic systems and target maneuvering, robust navigation guidance is required. Hence, a sliding mode control method is used for designing three-dimensional robust navigation guidance laws. Besides, parameters of sliding mode control are determined by minimizing multi-objective fitness function, which is the summation of the relative distance between missile-target and yaw angle of the line of sight. To show the effectiveness of the optimal sliding mode method, the simulation results are compared with some other techniques such as Proportional Navigation Guidance (PNG) and Augmented Proportional Navigation Guidance (APNG). It is proved that both the performance and efficiency of the proposed regulated-sliding-mode-based guidance scheme have significantly improved in comparison with these methods.

کلیدواژه‌ها [English]

  • Navigation-Guidance law
  • Sliding mode control
  • Harmony search algorithm
  • Robust Guidance

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سابقه مقاله

  • تاریخ دریافت: 07 خرداد 1398
  • تاریخ بازنگری: 12 تیر 1398
  • تاریخ پذیرش: 07 مرداد 1398
  • تاریخ انتشار: 01 فروردین 1399

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