IET Irish Signals and Systems Conference (ISSC 2008) 2008
DOI: 10.1049/cp:20080633
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State estimation for the VASIMR plasma engine

Abstract: This paper presents work on the application of virtual metrology techniques to the VAriable Specific Impulse Magnetoplasma Rocket (VASMIR) engine. The work concentrates on the estimation of internal temperatures of the rocket using state space models and Optical Emission Spectroscopy (OES). These estimations are useful as direct thermal measurements will not be available in the final system design.

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“…Such a potential drop of DL can accelerate ions downstream, achieving a kind of DL thruster [1][2][3][4]. For this reason, many researches have been carried out on the characteristics of DL [5][6][7][8][9][10][11] and the performance of helicon plasma thruster [12][13][14][15][16][17][18].…”
Section: Introductionmentioning
confidence: 99%
“…Such a potential drop of DL can accelerate ions downstream, achieving a kind of DL thruster [1][2][3][4]. For this reason, many researches have been carried out on the characteristics of DL [5][6][7][8][9][10][11] and the performance of helicon plasma thruster [12][13][14][15][16][17][18].…”
Section: Introductionmentioning
confidence: 99%