کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
---|---|---|---|---|
8057226 | 1520054 | 2018 | 11 صفحه PDF | دانلود رایگان |
عنوان انگلیسی مقاله ISI
Synthesis of attitude control for statically unstable hypersonic vehicle with low-frequency aero-servo-elastic effect
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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: Synthesis of attitude control for statically unstable hypersonic vehicle with low-frequency aero-servo-elastic effect Synthesis of attitude control for statically unstable hypersonic vehicle with low-frequency aero-servo-elastic effect](/preview/png/8057226.png)
چکیده انگلیسی
In this paper, an integrated attitude control scheme is proposed for a statically unstable hypersonic vehicle (HSV) with low-frequency aero-servo-elastic effect. Linear active disturbance rejection control (LADRC) is designed for the pitch angle to address the strong uncertainties and coupling effects. For the particular aero-servo-elastic effect with low frequency, a hybrid phase and gain stabilization technique is embedded into the LADRC framework to suppress the structural modes, which can reduce the phase loss around the crossover frequency. To achieve satisfactory tracking performance and robustness, a non-smooth Hâ optimization approach is applied to tune the controller gains, which simplifies the tuning and gain scheduling process. Monte Carlo simulation results demonstrate the effectiveness of the proposed control scheme.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Aerospace Science and Technology - Volume 80, September 2018, Pages 67-77
Journal: Aerospace Science and Technology - Volume 80, September 2018, Pages 67-77
نویسندگان
Minnan Piao, Zhihong Yang, Mingwei Sun, Jian Huang, Zenghui Wang, Zengqiang Chen,