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
fDate :
30 Oct-2 Nov 1988
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;
Conference_Titel :
Telecommunications Energy Conference, 1988. INTELEC '88., 10th International
Conference_Location :
San Diego, CA
DOI :
10.1109/INTLEC.1988.22354