Development of an advanced nano-satellite (VELOX-IV) : power supply system

The satellite research centre of NTU has successfully completed six satellite programs. Among them, VELOX-I and VELOX-II are classified as nano-satellites, i.e. satellites that weight between 1 and 50kg. For VELOX power supply system (PSS), it includes photovoltaic array (PV), battery management sys...

Full description

Saved in:
Bibliographic Details
Main Author: Sha, Lin
Other Authors: Low Kay Soon
Format: Final Year Project
Language:English
Published: 2016
Subjects:
Online Access:http://hdl.handle.net/10356/67724
Tags: Add Tag
No Tags, Be the first to tag this record!
Institution: Nanyang Technological University
Language: English
id sg-ntu-dr.10356-67724
record_format dspace
spelling sg-ntu-dr.10356-677242023-07-07T16:43:11Z Development of an advanced nano-satellite (VELOX-IV) : power supply system Sha, Lin Low Kay Soon School of Electrical and Electronic Engineering Satellite Engineering Centre DRNTU::Engineering The satellite research centre of NTU has successfully completed six satellite programs. Among them, VELOX-I and VELOX-II are classified as nano-satellites, i.e. satellites that weight between 1 and 50kg. For VELOX power supply system (PSS), it includes photovoltaic array (PV), battery management system (BMS) and power conversion and distribution (PCM/PDM) module. As with any power equipment, these systems are limited by the rated power. The maximum rated power of the step-down converter in VELOX-II is 30W or 6A. The objective of this final year project is to propose a modular power supply system (PSS) for a nano-satellite. The modular PSS can overcome the rated power limitation of equipment. This will help in reducing the development time further by allowing the scale-up of required power for future satellite programme. The proposed modular PSS consists of one power control module and several decision modules to implement power conversion/distribution and battery management functions. Each decision module of the PSS is controlled by single microcontroller and able to do decision making. The power control module is the brain of the whole PSS to control all decision modules. The control process is achieved through intra-satellite communication system. The controller area network (CAN) protocol is selected for the intra-satellite communication system due to its competency as compared with other communication types. The data transmission speed of the CAN bus is much higher and robust as compared to I2C and SPI. It reduces the wiring of the system significantly. All the messages from each module are transmitted through the CAN bus. The CAN message protocol is designed to make the PSS intelligent as every module can receive the correct message and discard the non-related or error message. The speed of the data transmission is up to 500Kbps which has been tested with the prototype implemented on the breadboard. The power conversion module is able to implement the MPPT function with efficiency of 86% and 83% by using P&O and InC algorithm respectively. The efficiency of the boost converter is approximately 87%. Testing is conducted at room temperature (25°C) by changing different parameters. Bachelor of Engineering 2016-05-19T07:57:11Z 2016-05-19T07:57:11Z 2016 Final Year Project (FYP) http://hdl.handle.net/10356/67724 en Nanyang Technological University 85 p. application/pdf
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic DRNTU::Engineering
spellingShingle DRNTU::Engineering
Sha, Lin
Development of an advanced nano-satellite (VELOX-IV) : power supply system
description The satellite research centre of NTU has successfully completed six satellite programs. Among them, VELOX-I and VELOX-II are classified as nano-satellites, i.e. satellites that weight between 1 and 50kg. For VELOX power supply system (PSS), it includes photovoltaic array (PV), battery management system (BMS) and power conversion and distribution (PCM/PDM) module. As with any power equipment, these systems are limited by the rated power. The maximum rated power of the step-down converter in VELOX-II is 30W or 6A. The objective of this final year project is to propose a modular power supply system (PSS) for a nano-satellite. The modular PSS can overcome the rated power limitation of equipment. This will help in reducing the development time further by allowing the scale-up of required power for future satellite programme. The proposed modular PSS consists of one power control module and several decision modules to implement power conversion/distribution and battery management functions. Each decision module of the PSS is controlled by single microcontroller and able to do decision making. The power control module is the brain of the whole PSS to control all decision modules. The control process is achieved through intra-satellite communication system. The controller area network (CAN) protocol is selected for the intra-satellite communication system due to its competency as compared with other communication types. The data transmission speed of the CAN bus is much higher and robust as compared to I2C and SPI. It reduces the wiring of the system significantly. All the messages from each module are transmitted through the CAN bus. The CAN message protocol is designed to make the PSS intelligent as every module can receive the correct message and discard the non-related or error message. The speed of the data transmission is up to 500Kbps which has been tested with the prototype implemented on the breadboard. The power conversion module is able to implement the MPPT function with efficiency of 86% and 83% by using P&O and InC algorithm respectively. The efficiency of the boost converter is approximately 87%. Testing is conducted at room temperature (25°C) by changing different parameters.
author2 Low Kay Soon
author_facet Low Kay Soon
Sha, Lin
format Final Year Project
author Sha, Lin
author_sort Sha, Lin
title Development of an advanced nano-satellite (VELOX-IV) : power supply system
title_short Development of an advanced nano-satellite (VELOX-IV) : power supply system
title_full Development of an advanced nano-satellite (VELOX-IV) : power supply system
title_fullStr Development of an advanced nano-satellite (VELOX-IV) : power supply system
title_full_unstemmed Development of an advanced nano-satellite (VELOX-IV) : power supply system
title_sort development of an advanced nano-satellite (velox-iv) : power supply system
publishDate 2016
url http://hdl.handle.net/10356/67724
_version_ 1772826150497681408