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http://dx.doi.org/10.5139/JKSAS.2006.34.1.095

On Stability of the Pulsed Plasma Thruster for STSAT-2 based on the Lyapunov Function  

Sin, Gu-Hwan (한국과학기술원)
Nam, Myeong-Yong (한국과학기술원)
Gang, Gyeong-In (한국과학기술원)
Im, Jong-Tae (한국과학기술원)
Cha, Won-Ho (한국과학기술원)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.34, no.1, 2006 , pp. 95-102 More about this Journal
Abstract
The PPT being currently developed for the flight model represents a significant leap in techniques and technology compared to the previous flight ones. The electrical energy to be charged in the pulsed plasma thruster (PPT) is a very important aspect to provide an uniform impulse bit ,, and a specific impulse ,, for satellite attitude control. In this paper, we propose a nonlinear control technique and a stability analysis based on the Lyapunov function for the pulsed plasma thruster. Specifically, the proposed control law guarantees to charge and discharge the electrical energy generated from the power processing unit (PPU) within the specified time.
Keywords
Impulse Bit, Specific Impulse, Pulsed Plasma Thruster, STSAT-2;
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