ATTITUDE CONTROL OF SUBORBITAL MODULE AND CHOOSING APPROPRIATE MODULATOR FOR SPATIAL APPLICATION

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MOUSAVI S.F.; EMAMI R.

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Paper Information

Journal: Journal of Aerospace Mechanics Year:2016 | Volume:11 | Issue:4 (42) (DYNAMICS, VIBRATIONS AND CONTROL) Page(s): 49-57

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Information Journal Paper

Title

ATTITUDE CONTROL OF SUBORBITAL MODULE AND CHOOSING APPROPRIATE MODULATOR FOR SPATIAL APPLICATION

Author(s)

MOUSAVI S.F. | EMAMI R. | Issue Writer Certificate

Keywords

ATTITUDE CONTROLQ2

REACTION CONTROL SYSTEMQ2

PWMQ2

PWPFQ2

Abstract

This paper is concerned with the design of an ATTITUDE CONTROL system for a suborbital module based on the pulse width and pulse width-pulse frequency modulators. The control algorithm is designed based on the quaternion error vector and performance of the two modulators is compared. Numerical simulation shows if parameters of PWPF modulator is tuned proper then the control effort decreases. Therefore this method proposed to implement in suborbital module.

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APA: Copy

MOUSAVI, S.F., & EMAMI, R.. (2016). ATTITUDE CONTROL OF SUBORBITAL MODULE AND CHOOSING APPROPRIATE MODULATOR FOR SPATIAL APPLICATION. AEROSPACE MECHANICS JOURNAL, 11(4 (42) (DYNAMICS, VIBRATIONS AND CONTROL)), 49-57. SID. https://sid.ir/paper/101993/en

Vancouver: Copy

MOUSAVI S.F., EMAMI R.. ATTITUDE CONTROL OF SUBORBITAL MODULE AND CHOOSING APPROPRIATE MODULATOR FOR SPATIAL APPLICATION. AEROSPACE MECHANICS JOURNAL[Internet]. 2016;11(4 (42) (DYNAMICS, VIBRATIONS AND CONTROL)):49-57. Available from: https://sid.ir/paper/101993/en

IEEE: Copy

S.F. MOUSAVI, and R. EMAMI, “ATTITUDE CONTROL OF SUBORBITAL MODULE AND CHOOSING APPROPRIATE MODULATOR FOR SPATIAL APPLICATION,” AEROSPACE MECHANICS JOURNAL, vol. 11, no. 4 (42) (DYNAMICS, VIBRATIONS AND CONTROL), pp. 49–57, 2016, [Online]. Available: https://sid.ir/paper/101993/en

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