Improved model of a partial shunt regulator for spacecraft

Author

Joung, G.B. ; Ma, K.S.

Author_Institution

Dept. of Inf. & Commun. Eng., Jeonbuk, South Korea

Volume

2

fYear

1997

fDate

26-29 May 1997

Firstpage

896

Abstract

The partial shunt regulator (PSR), which is a typical spacecraft power regulator, is modeled. To realize a simple structure, the voltage source of the PSR controller is identical to the output voltage of the PSR. However, the small-signal model structure of the PSR is very complex, because the PSR has a main feedback control loop as well as two additional coupled loops. The complex structure of model is simplified to a more meaningful structure, which has only one main feedback loop. The proposed PSR structure is verified by comparing the analysis of the model with SPICE simulation of the PSR circuit

Keywords

SPICE; aerospace computing; aerospace control; aerospace simulation; circuit analysis computing; control system analysis computing; feedback; space vehicle power plants; voltage control; voltage regulators; SPICE; circuit simulation; computer simulation; control simulation; feedback control loop; output voltage; partial shunt regulator; small-signal model structure; space power; spacecraft power supply; voltage source; Circuit simulation; Error correction; Feedback loop; Power amplifiers; Power system modeling; Power system reliability; Regulators; Space vehicles; Transfer functions; Voltage control;

fLanguage

English

Publisher

ieee

Conference_Titel

Power Electronics and Drive Systems, 1997. Proceedings., 1997 International Conference on

Print_ISBN

0-7803-3773-5

Type

conf

DOI

10.1109/PEDS.1997.627520

Filename

627520