NASA NTRS · 19760014190
Simulation of an ion thruster control system
Abstract
The results of an initial effort to model the control loops of a 30-cm diameter electron bombardment thruster and a transistorized power processor predicting its operation were described. Data from which the model is made is presented as well as comparisons between the computer outputs and test data from the JPL Solar Electric Propulsion systems laboratory.
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Kudo, I., Pless, L. C., Pawlik, E. V.. 1976-02-15. Simulation of an ion thruster control system. https://ntrs.nasa.gov/citations/19760014190
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