Modeling of an AC Power System for High Power Spacecraft

Details Modeling of an AC Power System for High Power Spacecraft Modeling of an AC Power System for High Power Spacecraft

Feb 2004

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2004aipc..699..598s&link_type=abstract

SPACE TECHNOLOGY AND APPLICATIONS INTERNAT.FORUM-STAIF 2004: Conf.on Thermophys.in Microgravity; Commercial/Civil Next Gen.Space

Statistics

Applications

Spaceborne And Space Research Instruments, Apparatus, And Components, Power Electronics, Power Supply Circuits

Scientific paper

This paper presents an analysis and simulation of an AC power system for a high power spacecraft that primarily supplies rectified loads. Two different configurations consisting of a three-phase PM synchronous generator and an associated power electronics converter are compared and analyzed. The first configuration consists of a three-phase PM synchronous generator and a three-phase diode bridge supplying a DC load. The second configuration consists of a three-phase PM synchronous generator and a three-phase PWM rectifier supplying the DC load. The modeling equations for both systems are derived. The comparisons between the two different configurations are summarized in a table in terms of efficiency, harmonic content and DC voltage ripple. The simulation results obtained by using SIMULINK are presented.

Affiliated with

Also associated with

No associations

Rating

Modeling of an AC Power System for High Power Spacecraft does not yet have a rating. At this time, there are no reviews or comments for this scientific paper.

If you have personal experience with Modeling of an AC Power System for High Power Spacecraft, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Modeling of an AC Power System for High Power Spacecraft will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFWR-SCP-O-1601371