کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
---|---|---|---|---|
7154015 | 1462495 | 2017 | 20 صفحه PDF | دانلود رایگان |
عنوان انگلیسی مقاله ISI
Non-fragile switched Hâ control for morphing aircraft with asynchronous switching
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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: Non-fragile switched Hâ control for morphing aircraft with asynchronous switching Non-fragile switched Hâ control for morphing aircraft with asynchronous switching](/preview/png/7154015.png)
چکیده انگلیسی
This paper deals with the problem of non-fragile linear parameter-varying (LPV) Hâ control for morphing aircraft with asynchronous switching. The switched LPV model of morphing aircraft is established by Jacobian linearization approach according to the nonlinear model. The data missing is taken into account in the link from sensors to controllers and the link from controllers to actuators, which satisfies Bernoulli distribution. The non-fragile switched LPV controllers are constructed with consideration of the uncertainties of controllers and asynchronous switching phenomenon. The parameter-dependent Lyapunov functional method and mode-dependent average dwell time (MDADT) method are combined to guarantee the stability and prescribed performance of the system. The sufficient conditions on the solvability of the problem are derived in the form of linear matrix inequalities (LMI). In order to achieve higher efficiency of the designing process, an algorithm is applied to divide the whole set into subsets automatically. Simulation results are provided to verify the effectiveness and superiority of the method in the paper.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Chinese Journal of Aeronautics - Volume 30, Issue 3, June 2017, Pages 1127-1139
Journal: Chinese Journal of Aeronautics - Volume 30, Issue 3, June 2017, Pages 1127-1139
نویسندگان
Haoyu CHENG, Chaoyang DONG, Weilai JIANG, Qing WANG, Yanze HOU,