کنترل ترکیبی PID-FUZZY پرواز آرایشمند فضاپیماها با هدف انحراف مسیر سیارک فضایی

نوع مقاله: مقالة‌ تحقیقی‌ (پژوهشی‌)

نویسندگان

1 دانشگاه صنعتی خواجه نصیر الدین طوسی

2 صنعتی خواجه نصیرالدین طوسی

چکیده

در این مقاله کنترل پرواز آرایشمند فضاپیماها با به کارگیری کنترل هیبریدی PID-FUZZY مورد بررسی قرار گرفته است. انحراف و تغییر مسیر سیارک‌های فضایی که باالقوه تهدیدی برای حیات بر روی کره زمین محسوب می‌گردند، در تحقیقات علمی اخیر به طور خیلی فعالی پیگیری می‌شود. برای انجام ماموریت مشروحه، تاکنون روش‌های متعددی پیشنهاد گردیده‌اند که در این بین استفاده از کشنده گرانشی شاخص می‌باشد و از این رو در مقاله حاضر از این روش بهره گرفته شده است. فناوری پرواز آرایشمند فضاپیماها تابع معادلات دینامک نسبیست که برای کنترل فعال آن نیز روش‌های گوناگونی به کار گرفته شده‌اند. در تحقیق پیش رو از کنترل کننده PID که کنترلی با کاربرد گسترده در صنایع گوناگون می‌باشد و ذاتا دارای خواص مقاوم بودن نیز هست، به عنوان کنترل کننده پایه بهره گرفته شده است و نیز برای بهبود تنظیم ضرایب آن از کنترل فازی استفاده شده که نتایج حاصله از شبیه سازی، بیانگر بهبود عملکرد کنترل کننده ترکیبی به طرزی موثر می‌باشد.

کلیدواژه‌ها


عنوان مقاله [English]

Hybrid PID-FUZZY Control of Formation Flying of Spacecrafts in order to asteroid Deflection Mission

نویسندگان [English]

  • Javad Shams 1
  • Jafar Roshanian 2
1 Khaje Nasir Toosi University of Technology
2 Khajeh Nasir Toosi UNIVERSITY OF TECHNOLOGY
چکیده [English]

In this paper, the hybrid control of the formation flying of spacecrafts has been investigated. The trajectory deflection of space asteroids, which are potentially life-threatening on Earth, are being actively pursued in recent scientific researches. To accomplish this mission, several methods have been proposed to date, in which case the use of gravity tractor is an indicator and hence the method is used in this paper. The formation flight of spacecrafts technology is a function of the relative dynamic equations, which are also used for its active control. In this way, the PID controller, which is widely used in various industries and inherently has robust properties, has been used as a base controller, and the fuzzy control has been used to improve its adjustment, which results in the results obtained. From simulation, the performance of the combined controller performance is effective.

کلیدواژه‌ها [English]

  • Asteroid Deflection
  • Asteroid Apophis
  • Spacecrafts Formation Flying
  • Relative Dynamic of Motion
  • Fuzzy logic
  • PID-FUZZY Controller
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