Please use this identifier to cite or link to this item: http://hdl.handle.net/11189/5784
Title: Electrical power system for a 3U CubeSat nanosatellite incorporating peak power tracking with dual redundant contro
Authors: Bester, Jean 
Groenewald, Ben BJ 
Wilkinson, R 
Keywords: CubeSat;Electrical power system;Peak power tracking;perturb & observe
Issue Date: 2012
Publisher: PRZEGLĄD ELEKTROTECHNICZNY
Source: Electrical Review, 04a: 300-304, 2012
Abstract: Since the advent of the CubeSat nanosatellite standard it has been embraced by many universities as an affordable means of conducting space science, with the backbone of any such mission being the supply of electrical power to the spacecraft’s payloads. This paper details the design of a photovoltaic-battery based power supply utilising peak power trackers for solar array regulation and battery charging. Uniquely, the peak power tracking is executed by an active search algorithm, Perturb & Observe, in both analogue and digital form as a measure of redundancy.
URI: http://hdl.handle.net/11189/5784
ISSN: 0033-2097
Appears in Collections:Eng - Journal articles (not DHET subsidised)

Files in This Item:
File Description SizeFormat 
Bester_J_Groenewald_BBJ_Wilkinson_R_Electrical power system for a 3U CubeSat _.pdfMain article542.86 kBAdobe PDFView/Open
Show full item record

Page view(s)

73
Last Week
0
Last month
7
checked on Jun 24, 2019

Download(s)

110
checked on Jun 24, 2019

Google ScholarTM

Check


This item is licensed under a Creative Commons License Creative Commons