کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
1715436 1519971 2012 9 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Fuzzy logic active flatness control of a space membrane structure
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مهندسی هوافضا
پیش نمایش صفحه اول مقاله
Fuzzy logic active flatness control of a space membrane structure
چکیده انگلیسی

This paper presents an experimental study on wrinkle reduction in a rectangular membrane structure with elliptical boundary cuts. The structure is subjected to two different heat loads: 145 °C and 205 °C. Wrinkling induced by the thermal expansion of the membrane is measured using a photogrammetry system and the root mean square of the membrane's surface above a plane of best fit. A fuzzy logic controller is developed to track a desired flatness level when the membrane is subject to either application or removal of a thermal load. Experimental verification is conducted using a membrane structure test facility and the results show that wrinkles have been reduced significantly and quickly using the proposed fuzzy logic controller.


► We perform experiments on a space rectangular membrane structure.
► The membrane is subjected to a varying thermal load creating flatness deviations.
► We design and implement a fuzzy logic controller for active flatness control.
► The controller enables a desired flatness level for the membrane to be tracked.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Acta Astronautica - Volume 77, August–September 2012, Pages 68–76
نویسندگان
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