An efficient method to control the amplitude of the limit cycle in satellite attitude control system

Sabet Rasekh, Mahdi; yadavar nikravesh, seyed kamaleddin; ghahramani, nematollah

دانشگاه صنعتی امیرکبیر

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An efficient method to control the amplitude of the limit cycle in satellite attitude control system

AUT Journal of Modeling and Simulation

مقاله 2، دوره 48، شماره 1، تابستان 2016، صفحه 13-27 اصل مقاله (1129 K)

نوع مقاله: Research Paper

شناسه دیجیتال (DOI): 10.22060/miscj.2016.634

نویسندگان

Mahdi Sabet Rasekh¹؛ seyed kamaleddin yadavar nikravesh

²؛ nematollah ghahramani³

¹Electrical engineering faculty Amirkabir university of technology

²Amirkabir University of technology

³Malek Ashtar University of technology

چکیده

In this paper, an efficient method is presented to control the attitude of a satellite with ON-OFF actuator. The main objective of this novel method is to control the amplitude of the limit cycle which commonly appears in the steady state of such systems; and at the same time by consideration of real actuator constraints, reduce the fuel consumption of system. The Proposed method is a combination of a command modifier (which based on the set point and the required accuracy of pointing, by means of optimization, calculate the desired limit cycle), a phase plane controller (PPC) and a compensator (to compensate for the real constraints of the actuator). The effectiveness and outperformance of the proposed method is approved in comparison with the previous methods of attitude control problem through the closed loop simulation and the stability and robustness of the closed loop system is fully analyzed and illustrated by simulations.

کلیدواژه ها

Limit Cycle؛ On/Off Actuator؛ Phase Plane Controller؛ Attitude Control؛ Robustness

عنوان مقاله [English]

An efficient method to control the amplitude of the limit cycle in satellite attitude control system

نویسندگان [English]

Mahdi Sabet Rasekh, seyed kamaleddin yadavar nikravesh, nematollah ghahramani

چکیده [English]

In this paper, an efficient method is presented to control the attitude of a satellite with ON-OFF actuator.
The main objective of this method is to control the amplitude of the limit cycle which commonly appears in
the steady state of such systems, while simultaneously by consideration of real actuator constraints, it
reduces the fuel consumption of system. The proposed method is a combination of a command modifier
(which is based on the set point and the required accuracy of pointing, by means of optimization, it calculates
the desired limit cycle), a phase plane controller (PPC) and a compensator (to compensate for the real
constraints of the actuator). The effectiveness and outperformance of the proposed method is approved in
comparison with the previous methods of attitude control problem through the closed loop simulation and the
stability and robustness of the closed loop system is fully analyzed and illustrated by simulations.

کلیدواژه ها [English]

Limit Cycle, On/Off Actuator, Phase Plane Controller, Attitude Control, Robustness

مراجع

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