کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
1718152 1520101 2013 6 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Robust fixed structure output feedback flight control law synthesis and analysis using singular structured value
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مهندسی هوافضا
پیش نمایش صفحه اول مقاله
Robust fixed structure output feedback flight control law synthesis and analysis using singular structured value
چکیده انگلیسی

This work proposes a method to design a fixed structure output feedback flight control law, joining flying qualities criterion with robustness to structured and unstructured uncertainties in the design specifications. The contribution is a straightforward design method to find simple control laws that comply with these specifications, using the structured singular value formulation. The method is applied to a typical pitch axis control problem, and analyzed from the robust control theory standpoint and a flying qualities criterion as well. The results show that the control law designed considering the uncertainties can provide better performance robustness than the design for the nominal plant.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Aerospace Science and Technology - Volume 30, Issue 1, October 2013, Pages 102–107
نویسندگان
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