PROVE OF STABILITY OF A SATELLITE INCLUDED MAGNETORQUERS AS ACTUATOR USING SLIDING CONTROL LAW

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.

GHORBANI VAGHEEI B.; BOLANDI H.

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

Journal Paper

Paper Information

Journal: JOURNAL OF FACULTY OF ENGINEERING (UNIVERSITY OF TABRIZ) Year:2003 | Volume:29 | Issue:1 (31 ELECTRICAL ENGINEERING) Page(s): 15-27

Download Full-Text

Persian Verion

View:

832

Download:

Cites:

Information Journal Paper

Title

PROVE OF STABILITY OF A SATELLITE INCLUDED MAGNETORQUERS AS ACTUATOR USING SLIDING CONTROL LAW

Author(s)

GHORBANI VAGHEEI B. | BOLANDI H. | Issue Writer Certificate

Keywords

DYNAMIC AND KINEMATIC EQUATION OF SPINNING SATELLITESQ2

MAGNETORQUERQ2

QUATERNIONQ2

SLIDING CONTROLQ2

Abstract

In general, most of satellites have nonlinear dynamic together with uncertainty and restricted constraints on their actuators. In this paper, stability of satellite by using SLIDING CONTROL as a robust control is proved in such a way that influences of above-mentioned limitations has been reduced. In this regard, after deriving dynamic and kinematic equation based on QUATERNION, sliding surface will be designed such that it will be stable. It is then illustrated that discrete SLIDING CONTROL law will not guarantee stability, but continuous one will guarantee satellite stability by proving. Finally, fine performance of designed control law is shown by simulation on a spinning satellite considering practical aspects.

Cites

No record.

References

DESIGN OF A NOVEL CONTROL LAW FOR SATELLITE BASED ON COMBINATION OF QUATERNION METHOD AND FEEDBACK LINEARIZATION LAW

Cite

APA: Copy

GHORBANI VAGHEEI, B., & BOLANDI, H.. (2003). PROVE OF STABILITY OF A SATELLITE INCLUDED MAGNETORQUERS AS ACTUATOR USING SLIDING CONTROL LAW. JOURNAL OF FACULTY OF ENGINEERING (UNIVERSITY OF TABRIZ), 29(1 (31 ELECTRICAL ENGINEERING)), 15-27. SID. https://sid.ir/paper/43777/en

Vancouver: Copy

GHORBANI VAGHEEI B., BOLANDI H.. PROVE OF STABILITY OF A SATELLITE INCLUDED MAGNETORQUERS AS ACTUATOR USING SLIDING CONTROL LAW. JOURNAL OF FACULTY OF ENGINEERING (UNIVERSITY OF TABRIZ)[Internet]. 2003;29(1 (31 ELECTRICAL ENGINEERING)):15-27. Available from: https://sid.ir/paper/43777/en

IEEE: Copy

B. GHORBANI VAGHEEI, and H. BOLANDI, “PROVE OF STABILITY OF A SATELLITE INCLUDED MAGNETORQUERS AS ACTUATOR USING SLIDING CONTROL LAW,” JOURNAL OF FACULTY OF ENGINEERING (UNIVERSITY OF TABRIZ), vol. 29, no. 1 (31 ELECTRICAL ENGINEERING), pp. 15–27, 2003, [Online]. Available: https://sid.ir/paper/43777/en

Related Journal Papers