Cube Satellite Battery Charger Regulator Design-Reference-Cited by-同舟云学术

Cube Satellite Battery Charger Regulator Design

Published:2022-12-31 Issue: Volume:13 Page:142-146
ISSN:2415-1513
Container-title:WSEAS TRANSACTIONS ON ELECTRONICS
language:en
Short-container-title:

Author:

Metehri Fethi¹,Bensaada Messaoud¹,Beldjehem Mohammed¹

Affiliation:

1. Algerian Space Agency, Centre for Satellites Development, Oran, ALGERIA

Abstract

Battery Charger Regulator (BCR) circuit used on spacecraft power systems, are usually switching regulators to provide maximum power for current operation mode and fixed voltage for voltage mode. In this article, we present detailed design procedures for BCR implemented on Cube-satellite. We will show small-signal analysis of a battery charger, to perform the control loop design of the maximum power point detection step and also voltage mode control loop to detecte battery Endof- charge. We present also a simulation of tow loops to verify our design.

Publisher

World Scientific and Engineering Academy and Society (WSEAS)

Subject

Electrical and Electronic Engineering

Reference10 articles.

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3. Craig S. Clark 2002 “Universal Power System Archtecture: One Topology For Earth and Planetary Orbits” Journal Space power system ESA SP-502, ,page.135.

4. Daniel M. All, Evaluation of Solar Array Peak Tracking Tchnology For Cubesat “ 25th Annual AIAA/USU conference on small satellite.

5. Grant Bonin, Al Peak Power Tracking On a Nanosatellite Scale: The design and Implementation of Digital Power Electronics on the SFL Geniric Nanosatellite Bus.

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