کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
---|---|---|---|---|
560934 | 875226 | 2006 | 23 صفحه PDF | دانلود رایگان |
عنوان انگلیسی مقاله ISI
Control of an all-movable foreplane for a three surfaces aircraft wind tunnel model
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کلمات کلیدی
موضوعات مرتبط
مهندسی و علوم پایه
مهندسی کامپیوتر
پردازش سیگنال
پیش نمایش صفحه اول مقاله
![عکس صفحه اول مقاله: Control of an all-movable foreplane for a three surfaces aircraft wind tunnel model Control of an all-movable foreplane for a three surfaces aircraft wind tunnel model](/preview/png/560934.png)
چکیده انگلیسی
This article deals with design and realisation of a canard foreplane control system for an aeroelastic demonstrator, suitable for wind tunnel testing. Hardware and software will be described as the methodology adopted to design, implement and realise the software. Specific attention is devoted to PID application, tuning and fuselage vibration control implementation. Results of preliminary test and simulations are presented and show realistic system effectiveness in damping fuselage bending and torsion. This work describes all the activity performed at Politecnico di Milano before wind tunnel testing at VZLU, Prague, as part of Active Aeroelastic Aircraft Structures (3AS) EU project.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Mechanical Systems and Signal Processing - Volume 20, Issue 5, July 2006, Pages 1044–1066
Journal: Mechanical Systems and Signal Processing - Volume 20, Issue 5, July 2006, Pages 1044–1066
نویسندگان
S. Ricci, A. Scotti, D. Zanotti,