کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
---|---|---|---|---|
1718188 | 1013832 | 2013 | 12 صفحه PDF | دانلود رایگان |
عنوان انگلیسی مقاله ISI
Estimation of maneuvering aircraft states and time-varying wind with turbulence
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کلمات کلیدی
موضوعات مرتبط
مهندسی و علوم پایه
سایر رشته های مهندسی
مهندسی هوافضا
پیش نمایش صفحه اول مقاله
![عکس صفحه اول مقاله: Estimation of maneuvering aircraft states and time-varying wind with turbulence Estimation of maneuvering aircraft states and time-varying wind with turbulence](/preview/png/1718188.png)
چکیده انگلیسی
This paper presents an application of the Square Root-Unscented Kalman Filter (SR-UKF) to the estimation of aircraft system states and to the estimation of the total wind vector made up of a time-varying prevailing wind plus turbulence. The estimates are computed using conventional auto-pilot sensors with exponentially correlated measurement errors. The objective of this work is to investigate the convergence limitations of the estimates considering the covariance and correlation time constants of the measurement error models as well as the level of intensity of the turbulence.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Aerospace Science and Technology - Volume 31, Issue 1, December 2013, Pages 87–98
Journal: Aerospace Science and Technology - Volume 31, Issue 1, December 2013, Pages 87–98
نویسندگان
Je Hyeon Lee, Hakki Erhan Sevil, Atilla Dogan, David Hullender,