ATTITUDE STABILIZATION AND MANAUVRING OF AGILITY NANOSATELLITE WITH CONTROL MOMENT GYROS

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.

NIKKHAH A.A.; Tayyebi J.; ROSHANIYAN J.

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:2014 | Volume:7 | Issue:2 Page(s): 1-9

Download Full-Text

Persian Verion

View:

765

Download:

Cites:

Information Journal Paper

Title

ATTITUDE STABILIZATION AND MANAUVRING OF AGILITY NANOSATELLITE WITH CONTROL MOMENT GYROS

Author(s)

NIKKHAH A.A. | Tayyebi J. | ROSHANIYAN J. | Issue Writer Certificate

Keywords

SATELLITE ATTITUDE CONTROLQ2

AGILITY SATELLITEQ2

CONTROL MOMENT GYROSCOPE (CMG)Q2

STEERING OF CMGQ2

SINGULARITY CONDITIONQ2

LQGQ2

LQRQ2

Abstract

In this paper attitude control system of nanosatellite based on Single Gimbal Control Moment Gyroscope (SGCMG) is presented. A LQR/LQG method is developed for stability of satellite and a feedback quaternion strategy is used for maneuvering mode. In the stabilization mode LQR/LQG controllers are designed with linearization of nonlinear dynamic equation of satellite and control moment gyroscope, so that in other reseach didn’t use this controller in the stabilization mode of this system. In the maneuvering mode a feedback quaternion controller applyed for nonlinear system. Numerical simulations are provided to show the efficiency of the proposed controller for a nanosatellite with four single gimbal control moment gyroscope pyramid cluster. Results of simulations shown that LQR/LQG method is more accurate in compared with feedback quaternion controller.

Cites

No record.

References

No record.

Cite

APA: Copy

NIKKHAH, A.A., Tayyebi, J., & ROSHANIYAN, J.. (2014). ATTITUDE STABILIZATION AND MANAUVRING OF AGILITY NANOSATELLITE WITH CONTROL MOMENT GYROS. JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST), 7(2 ), 1-9. SID. https://sid.ir/paper/149929/en

Vancouver: Copy

NIKKHAH A.A., Tayyebi J., ROSHANIYAN J.. ATTITUDE STABILIZATION AND MANAUVRING OF AGILITY NANOSATELLITE WITH CONTROL MOMENT GYROS. JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST)[Internet]. 2014;7(2 ):1-9. Available from: https://sid.ir/paper/149929/en

IEEE: Copy

A.A. NIKKHAH, J. Tayyebi, and J. ROSHANIYAN, “ATTITUDE STABILIZATION AND MANAUVRING OF AGILITY NANOSATELLITE WITH CONTROL MOMENT GYROS,” JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST), vol. 7, no. 2 , pp. 1–9, 2014, [Online]. Available: https://sid.ir/paper/149929/en

Related Journal Papers