Design of a Conntroller for Using MEMS Vibrational Gyroscope System

Q: How can I download an article?

To download an article from SID, first log in to the site, search for the article title, and click on the 'Download Article' option.

Q: How can I download an ISI article?

To download an ISI article on SID, enter the keyword or article title in the search bar, view the relevant results, click on the desired article, and select the 'Download Article' option.

Q: How can I access the SID database?

To access the SID database, visit SID.ir, create an account, and log in to access scientific resources.

Q: Is downloading articles from SID free?

Some articles on SID are available for free, while others require payment. Details are specified on the article's page.

SOLTANPOUR M.R.; KHAKI R.

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Journal Paper

Paper Information

Journal: Journal of Aerospace Mechanics Year:2019 | Volume:15 | Issue:3 Page(s): 1-16

Download Full-Text

Persian Verion

View:

430

Download:

Cites:

Information Journal Paper

Title

Design of a Conntroller for Using MEMS Vibrational Gyroscope System

Author(s)

SOLTANPOUR M.R. | KHAKI R. | Issue Writer Certificate

Keywords

MEMS Vibrational GyroscopeQ1

Terminal Sliding Mode ControlQ1

UncertaintyQ2

Adaptive EstimatorQ1

Adaptive Terminal Sliding Mode ControlQ1

ChatteringQ1

Abstract

An adaptive Terminal Sliding Mode Control scheme is presented for Micro-Electro-Mechanical Systems (MEMS) vibrational gyroscope system in this paper. In this approach the dynamics of the vibrational gyroscope system is eliminated by using inverse dynamic method to reduce the bounds of existing uncertainties. the designed Terminal Sliding Mode Control vector is provided a global asymptotic stability for close loop system with uncertainties. In this paper, an Adaptive Estimator is proposed to prevent the occurrence of a Chattering problem at the control input, which has only one law. The mathematical proof shows that the closed loop system, with proposed adaptive Terminal Sliding Mode Controller with uncertainties has a global asymptotic stability. Four-phase simulations are implemented on the MEMS Vibrational Gyroscope system to demonstrate the performance of the controller and compare it with other similar controllers. The simulation results show that the proposed adaptive Terminal Sliding Mode Controller has desired performance.

Cites

No record.

References

No record.

Cite

APA: Copy

SOLTANPOUR, M.R., & KHAKI, R.. (2019). Design of a Conntroller for Using MEMS Vibrational Gyroscope System. AEROSPACE MECHANICS JOURNAL, 15(3 ), 1-16. SID. https://sid.ir/paper/101690/en

Vancouver: Copy

SOLTANPOUR M.R., KHAKI R.. Design of a Conntroller for Using MEMS Vibrational Gyroscope System. AEROSPACE MECHANICS JOURNAL[Internet]. 2019;15(3 ):1-16. Available from: https://sid.ir/paper/101690/en

IEEE: Copy

M.R. SOLTANPOUR, and R. KHAKI, “Design of a Conntroller for Using MEMS Vibrational Gyroscope System,” AEROSPACE MECHANICS JOURNAL, vol. 15, no. 3 , pp. 1–16, 2019, [Online]. Available: https://sid.ir/paper/101690/en

Related Journal Papers