کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
---|---|---|---|---|
758087 | 1462552 | 2007 | 7 صفحه PDF | دانلود رایگان |
عنوان انگلیسی مقاله ISI
Gain Scheduling Control of Nonlinear Shock Motion Based on Equilibrium Manifold Linearization Model
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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: Gain Scheduling Control of Nonlinear Shock Motion Based on Equilibrium Manifold Linearization Model Gain Scheduling Control of Nonlinear Shock Motion Based on Equilibrium Manifold Linearization Model](/preview/png/758087.png)
چکیده انگلیسی
The equilibrium manifold linearization model of nonlinear shock motion is of higher accuracy and lower complexity over other models such as the small perturbation model and the piecewise-linear model. This paper analyzes the physical significance of the equilibrium manifold linearization model, and the self-feedback mechanism of shock motion is revealed. This helps to describe the stability and dynamics of shock motion. Based on the model, the paper puts forwards a gain scheduling control method for nonlinear shock motion. Simulation has shown the validity of the control scheme.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Chinese Journal of Aeronautics - Volume 20, Issue 6, December 2007, Pages 481-487
Journal: Chinese Journal of Aeronautics - Volume 20, Issue 6, December 2007, Pages 481-487