کنترل فعال ارتعاشات و پایدارسازی مقاوم چند جسمی صلب-انعطاف ‏پذیر با الگوریتم مود لغزشی زمان متغیر

نوع مقاله : گرایش دینامیک، ارتعاشات و کنترل

نویسنده

استادیار، پژوهشکده سامانه‌های فضانوردی، پژوهشگاه هوافضا (وزارت علوم، تحقیقات و فناوری)، تهران، ایران

چکیده

در این مقاله به طراحی کنترلرهای مقاوم هیبرید مود لغزشی توسعه‌یافته با سطح لغزش زمان متغیر و ارتعاشات یک فضاپیمای انعطاف‏پذیر در مانور وضعیت پرداخته‌شده‌ است. مدل دینامیک غیرخطی کاملاً کوپل صلب-انعطاف‏پذیر شامل دوران سه محوره جسم صلب در تعامل با تغییرشکل‏های عرضی پنل‏های انعطاف‏پذیر مجهز به حسگر/عملگر‏های پیزوالکتریک می‏باشد. سیگنال هموار کنترلی شامل ترم تانژانت هایپربولیک و یک تابع تنظیم شدت‏ سوئیچینگ به‌منظور کاهش اثرات چترینگ و تعدیل اثرات ناشی از تعاملات فرکانس بالای بخش‏های انعطاف‏پذیر و اغتشاشات خارجی با بدنه صلب و کنترلر می‏باشد. ساختار سطح لغزشی متغیر با زمان امکان تنظیم میزان اثر پارامترهای وضعیت (کواترنیون‏ها و سرعت‏های زاویه‏ای) را بر عملکرد کنترلی فراهم ساخته است. همچنین ارتعاشات باقی‏مانده حین و پس از فاز دستیابی به هدف با به‌کارگیری یک الگوریتم مقاوم کنترل فعال ارتعاشات، کاهش‌یافته است. شبیه‏سازی‏ها در قالب مطالعه مقایسه‏ای، عملکرد و برتری رویکرد پیشنهادی را در مقایسه با رویکرد کلاسیک کنترل مود لغزشی برای سیستم‏های با انعطاف‏پذیری سازه‏ای در حضور اغتشاشات خارجی و نامعینی‏ها نمایش می‏دهد.

کلیدواژه‌ها


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دوره 18، شماره 4 - شماره پیاپی 70
شماره پیاپی 70، فصلنامه زمستان
دی 1401
صفحه 49-63
  • تاریخ دریافت: 12 تیر 1401
  • تاریخ بازنگری: 06 مرداد 1401
  • تاریخ پذیرش: 23 مرداد 1401
  • تاریخ انتشار: 01 دی 1401