کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
---|---|---|---|---|
1719020 | 1013885 | 2006 | 10 صفحه PDF | دانلود رایگان |
عنوان انگلیسی مقاله ISI
A systematic single-range controller synthesis procedure for nonlinear and multivariable liquid propellant engines
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موضوعات مرتبط
مهندسی و علوم پایه
سایر رشته های مهندسی
مهندسی هوافضا
پیش نمایش صفحه اول مقاله
![عکس صفحه اول مقاله: A systematic single-range controller synthesis procedure for nonlinear and multivariable liquid propellant engines A systematic single-range controller synthesis procedure for nonlinear and multivariable liquid propellant engines](/preview/png/1719020.png)
چکیده انگلیسی
A new systematic single-range controller synthesis procedure for use with nonlinear, multivariable, and time-varying liquid propellant engines is developed. The developed procedure is based on one describing function model of the nonlinear plant coupled with two different linear algebraic controller design procedures; one of the algebraic procedures is to achieve decoupling, and the second one is to achieve command following. The developed procedure is demonstrated by solving an example problem comparing the results using a H∞ controller design procedure.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Aerospace Science and Technology - Volume 10, Issue 5, July 2006, Pages 401-410
Journal: Aerospace Science and Technology - Volume 10, Issue 5, July 2006, Pages 401-410