SATELLITE ADAPTIVE ATTITUDE CONTROL BASED ON DECENTRALIZED MINIMAL CONTROL IN THE PRESENCE OF REACTION WHEEL ACCURATE MODEL

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.

SAMADI KHOSHKHO Z.; MORTAZAVI BEK M.; FANI SABERI F.

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:2016 | Volume:9 | Issue:1 Page(s): 47-57

Download Full-Text

Persian Verion

View:

1,215

Download:

Cites:

Information Journal Paper

Title

SATELLITE ADAPTIVE ATTITUDE CONTROL BASED ON DECENTRALIZED MINIMAL CONTROL IN THE PRESENCE OF REACTION WHEEL ACCURATE MODEL

Author(s)

SAMADI KHOSHKHO Z. | MORTAZAVI BEK M. | FANI SABERI F. | Issue Writer Certificate

Keywords

ADAPTIVE ATTITUDE CONTROLQ1

REACTION WHEEL MODELQ1

SATELLITEQ2

UNCERTAINTY AND ACTUATOR SATURATIONQ2

Abstract

In this paper, an adaptive controller based on decentralized minimal control synthesis is designed n order to control an attitude of specific remote sensing SATELLITE. The main design purposes are performing spinning, three axis and large angle maneuver as well as achieving a stable system and tracking the reference attitude trajectory in the presence of uncertainties. In the design process, the effects of internal and external disturbances, nonlinearities in the SATELLITE dynamic and the accurate model of actuators are regarded. Four reaction wheels with pyramidal structure are modeled as the actuators to accomplish an attitude maneuver. So the exact reaction wheels’ model with regarding the maximum voltage, current, allowable angular velocities and power of wheels is developed. The simulation results show an acceptable performance of controller in the presence of exacts actuators’ model, external and internal disturbances and uncertainties in the SATELLITE parameters.

Cites

No record.

References

No record.

Cite

APA: Copy

SAMADI KHOSHKHO, Z., MORTAZAVI BEK, M., & FANI SABERI, F.. (2016). SATELLITE ADAPTIVE ATTITUDE CONTROL BASED ON DECENTRALIZED MINIMAL CONTROL IN THE PRESENCE OF REACTION WHEEL ACCURATE MODEL. JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST), 9(1), 47-57. SID. https://sid.ir/paper/149944/en

Vancouver: Copy

SAMADI KHOSHKHO Z., MORTAZAVI BEK M., FANI SABERI F.. SATELLITE ADAPTIVE ATTITUDE CONTROL BASED ON DECENTRALIZED MINIMAL CONTROL IN THE PRESENCE OF REACTION WHEEL ACCURATE MODEL. JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST)[Internet]. 2016;9(1):47-57. Available from: https://sid.ir/paper/149944/en

IEEE: Copy

Z. SAMADI KHOSHKHO, M. MORTAZAVI BEK, and F. FANI SABERI, “SATELLITE ADAPTIVE ATTITUDE CONTROL BASED ON DECENTRALIZED MINIMAL CONTROL IN THE PRESENCE OF REACTION WHEEL ACCURATE MODEL,” JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST), vol. 9, no. 1, pp. 47–57, 2016, [Online]. Available: https://sid.ir/paper/149944/en

Related Journal Papers