DEIGNING SPACECRAFT ATTITUDE CONTROL USING MODEL-FREE OPTIMAL CONTROL THEORY

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.

TAJI HERVI FARID; NOVINZADEH ALIREZA

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

Journal Paper

Paper Information

Journal: Journal of Space Science and Technology Year:2017 | Volume:10 | Issue:3 Page(s): 41-57

Download Full-Text

Persian Verion

View:

1,485

Download:

Cites:

Information Journal Paper

Title

DEIGNING SPACECRAFT ATTITUDE CONTROL USING MODEL-FREE OPTIMAL CONTROL THEORY

Author(s)

TAJI HERVI FARID | NOVINZADEH ALIREZA | Issue Writer Certificate

Keywords

DYNAMIC PROGRAMMINGQ1

LINEAR QUADRATIC REGULATORQ1

MODEL-FREE CONTROLLERQ1

ATTITUDE CONTROL OF SPACECRAFTQ2

Abstract

The purpose of the present paper is to prove the model-free optimal control theory. This theory is derived from the principles of DYNAMIC PROGRAMMING and it is produced for discrete-time systems. The design of the controller depends merely on the I/O data of the controlled planet; hence, the controller is independent of the model. In this paper, two actions have been performed in order to measure the value of the controller. In the first step, the control method was designed to control the attitude of spacecraft. The purpose of this theory was to create a model-free optimal control for the spatial model and to measure the efficiency of the spacecraft systems. Secondly, designing LINEAR QUADRATIC REGULATOR (LQR) controller for ATTITUDE CONTROL OF SPACECRAFT was carried out. The reason for designing this controller was to compare it with model-free optimal control. If the differences between two controllers was proved to be small, then the theory would be proven. Finally, it has been concluded that controller is valuable and acceptable.

Cites

No record.

References

No record.

Cite

APA: Copy

TAJI HERVI, FARID, & NOVINZADEH, ALIREZA. (2017). DEIGNING SPACECRAFT ATTITUDE CONTROL USING MODEL-FREE OPTIMAL CONTROL THEORY. JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST), 10(3 ), 41-57. SID. https://sid.ir/paper/149949/en

Vancouver: Copy

TAJI HERVI FARID, NOVINZADEH ALIREZA. DEIGNING SPACECRAFT ATTITUDE CONTROL USING MODEL-FREE OPTIMAL CONTROL THEORY. JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST)[Internet]. 2017;10(3 ):41-57. Available from: https://sid.ir/paper/149949/en

IEEE: Copy

FARID TAJI HERVI, and ALIREZA NOVINZADEH, “DEIGNING SPACECRAFT ATTITUDE CONTROL USING MODEL-FREE OPTIMAL CONTROL THEORY,” JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST), vol. 10, no. 3 , pp. 41–57, 2017, [Online]. Available: https://sid.ir/paper/149949/en

Related Journal Papers