Gliding-Guided Projectile Attitude Tracking Controller Design Based on Improved Adaptive Twisting Sliding Mode Algorithm

المؤلفون المشاركون

Zhang, Wenguang
Yi, Wenjun

المصدر

International Journal of Aerospace Engineering

العدد

المجلد 2020، العدد 2020 (31 ديسمبر/كانون الأول 2020)، ص ص. 1-15، 15ص.

الناشر

Hindawi Publishing Corporation

تاريخ النشر

2020-10-31

دولة النشر

مصر

عدد الصفحات

15

الملخص EN

The finite-time attitude tracking control for gliding-guided projectile with unmatched and matched disturbance is investigated.

An adaptive variable observer is used to provide estimation for the unmeasured state which contains unmatched disturbance.

Then, an improved adaptive twisting sliding mode algorithm is proposed to compensate for the matched disturbance dynamically with better transient quality.

Finally, a proof of the finite-time convergence of the closed-loop system under the disturbance observer and the adaptive twisting sliding mode-based controller is derived using the Lyapunov technique.

This attitude tracking control scheme does not require any information on the bounds of uncertainties.

Simulation results demonstrate that the proposed method which is able to acquire the minimum possible values of the control gains guaranteeing the finite-time convergence performs well in chattering attenuation and tracking precision.

نمط استشهاد جمعية علماء النفس الأمريكية (APA)

Zhang, Wenguang& Yi, Wenjun. 2020. Gliding-Guided Projectile Attitude Tracking Controller Design Based on Improved Adaptive Twisting Sliding Mode Algorithm. International Journal of Aerospace Engineering،Vol. 2020, no. 2020, pp.1-15.
https://search.emarefa.net/detail/BIM-1167947

نمط استشهاد الجمعية الأمريكية للغات الحديثة (MLA)

Zhang, Wenguang& Yi, Wenjun. Gliding-Guided Projectile Attitude Tracking Controller Design Based on Improved Adaptive Twisting Sliding Mode Algorithm. International Journal of Aerospace Engineering No. 2020 (2020), pp.1-15.
https://search.emarefa.net/detail/BIM-1167947

نمط استشهاد الجمعية الطبية الأمريكية (AMA)

Zhang, Wenguang& Yi, Wenjun. Gliding-Guided Projectile Attitude Tracking Controller Design Based on Improved Adaptive Twisting Sliding Mode Algorithm. International Journal of Aerospace Engineering. 2020. Vol. 2020, no. 2020, pp.1-15.
https://search.emarefa.net/detail/BIM-1167947

نوع البيانات

مقالات

لغة النص

الإنجليزية

الملاحظات

Includes bibliographical references

رقم السجل

BIM-1167947