EFFECT OF TRANSFER FUNCTION ORDER OF THRUSTER ACTUATORS ON SATELLITE ATTITUDE CONTROL

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.

JALALI NAINI S.H.; KHALILI N.

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

Journal Paper

Paper Information

Journal: Journal of Aerospace Mechanics Year:2016 | Volume:11 | Issue:4 (42) (DYNAMICS, VIBRATIONS AND CONTROL) Page(s): 59-71

Download Full-Text

Persian Verion

View:

1,421

Download:

Cites:

Information Journal Paper

Title

EFFECT OF TRANSFER FUNCTION ORDER OF THRUSTER ACTUATORS ON SATELLITE ATTITUDE CONTROL

Author(s)

JALALI NAINI S.H. | KHALILI N. | Issue Writer Certificate

Keywords

THRUSTER DYNAMICSQ2

BANG-BANG CONTROLLERQ2

SCHMITT-TRIGGERQ2

PULSE WIDTH-PULSE FREQUENCY MODULATIONQ2

Abstract

In this paper, effect of order of the thruster transfer function is investigated for a single-axis attitude control of a rigid satellite using two sets of opposing thrusters. The THRUSTER DYNAMICS is modeled by a pure delay in series with an arbitrary-order transfer function (TF) consisting of similar first-order lags. For this purpose, BANG-BANG CONTROLLERs, bang-bang with dead zone, SCHMITT-TRIGGER and PWPF modulator are used in the analysis. The THRUSTER DYNAMICS order is selected using existing empirical thruster profiles. Considering the empirical profiles, usually a TF’s order lower than 2 is not recommended. Simulation results show that the TF’s order may be considered as an uncertainty applied to the attitude control problem and its sensitivity analysis.

Cites

No record.

References

No record.

Cite

APA: Copy

JALALI NAINI, S.H., & KHALILI, N.. (2016). EFFECT OF TRANSFER FUNCTION ORDER OF THRUSTER ACTUATORS ON SATELLITE ATTITUDE CONTROL. AEROSPACE MECHANICS JOURNAL, 11(4 (42) (DYNAMICS, VIBRATIONS AND CONTROL)), 59-71. SID. https://sid.ir/paper/101989/en

Vancouver: Copy

JALALI NAINI S.H., KHALILI N.. EFFECT OF TRANSFER FUNCTION ORDER OF THRUSTER ACTUATORS ON SATELLITE ATTITUDE CONTROL. AEROSPACE MECHANICS JOURNAL[Internet]. 2016;11(4 (42) (DYNAMICS, VIBRATIONS AND CONTROL)):59-71. Available from: https://sid.ir/paper/101989/en

IEEE: Copy

S.H. JALALI NAINI, and N. KHALILI, “EFFECT OF TRANSFER FUNCTION ORDER OF THRUSTER ACTUATORS ON SATELLITE ATTITUDE CONTROL,” AEROSPACE MECHANICS JOURNAL, vol. 11, no. 4 (42) (DYNAMICS, VIBRATIONS AND CONTROL), pp. 59–71, 2016, [Online]. Available: https://sid.ir/paper/101989/en

Related Journal Papers