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

Joint Authors

Zhang, Wenguang
Yi, Wenjun

Source

International Journal of Aerospace Engineering

Issue

Vol. 2020, Issue 2020 (31 Dec. 2020), pp.1-15, 15 p.

Publisher

Hindawi Publishing Corporation

Publication Date

2020-10-31

Country of Publication

Egypt

No. of Pages

15

Abstract 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.

American Psychological Association (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

Modern Language Association (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

American Medical Association (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

Data Type

Journal Articles

Language

English

Notes

Includes bibliographical references

Record ID

BIM-1167947