Attitude Control of Satellite with PWPF Modulator Using Generalized Incremental Predictive Control
سال انتشار: 1394
نوع سند: مقاله ژورنالی
زبان: انگلیسی
مشاهده: 459
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شناسه ملی سند علمی:
JR_JKBEI-1-2_005
تاریخ نمایه سازی: 17 شهریور 1395
چکیده مقاله:
In this paper, we use generalized incremental predictive control to stabilize attitude of satellite. We compare GPC with GIPC algorithm and present that GIPC has better performance. The three-axis attitude control systems are activated in pulse mode. Consequently, a modulation of the torque command is compelling in order to avoid high non-linear control action. This work considers the Pulse-Width Pulse-Frequency modulator is composed of a Schmitt trigger, a first order filter, and a feedback loop. PWPF modulator has several advantages over classical bang-bang controllers such as close to linear operation, high accuracy, and reduced propellant consumption
کلیدواژه ها:
نویسندگان
Ehsan Chegeni
Department of Control Engineering Islamic Azad University, Science and Research Boroujerd Branch, Iran
Saeed Mohamad Hoseini
Department of Control Engineering Islamic Azad University, Science and Research Boroujerd Branch, Iran
m Madadpour Inallou
Young Researchers and Elites Club, West Tehran Branch, Islamic Azad University, Tehran, Iran