DocumentCode
3209033
Title
A high frequency, multi-module, spacecraft boost regulator
Author
Sable, D.M. ; Ridley, R.B.
Author_Institution
Virginia Power Electron. Center, Virginia Polytech. Inst. & State Univ., Blacksburg, VA, USA
fYear
1988
fDate
30 Oct-2 Nov 1988
Firstpage
227
Lastpage
235
Abstract
The design of a high-frequency, multimodule boost regulator suitable for use as a spacecraft battery discharger is presented. A combination of AC inductor current feedback and current-injection (DC switch current feedback) is used for optimum dynamic performance, overload protection, noise immunity, and current sharing of the modules. By suitable design of the second stage output filter, it is shown that the output impedance characteristic possesses a resonant notch instead of a resonant peak and can ensure system stability over a wide range of complex load conditions. Both the overall loop gain and the outer loop gain must be viewed to fully understand all system dynamics
Keywords
controllers; feedback; space vehicle power plants; AC inductor current feedback; DC switch current feedback; HF multimodule spacecraft boost regulator; current sharing; dynamic performance; noise immunity; outer loop gain; output impedance characteristic; overall loop gain; overload protection; spacecraft battery discharger; stability; Batteries; Feedback; Filters; Frequency; Inductors; Protection; Regulators; Resonance; Space vehicles; Switches;
fLanguage
English
Publisher
ieee
Conference_Titel
Telecommunications Energy Conference, 1988. INTELEC '88., 10th International
Conference_Location
San Diego, CA
Type
conf
DOI
10.1109/INTLEC.1988.22354
Filename
22354
Link To Document