CanSat, satellite in a soda can

This report documents the development of a CanSat from scratch to a working prototype. The first CanSat project is initiated in 1999 named, A Rocket Launch for International Student Satellites (ARLISS). It is a collaborative effort with faculty of Stanford University Space Systems Development Progra...

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Main Author: Koh, Jian Cheng
Other Authors: Ling Keck Voon
Format: Final Year Project
Language:English
Published: 2014
Subjects:
Online Access:http://hdl.handle.net/10356/59275
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-592752023-07-07T17:12:47Z CanSat, satellite in a soda can Koh, Jian Cheng Ling Keck Voon School of Electrical and Electronic Engineering Satellite Engineering Centre DRNTU::Engineering This report documents the development of a CanSat from scratch to a working prototype. The first CanSat project is initiated in 1999 named, A Rocket Launch for International Student Satellites (ARLISS). It is a collaborative effort with faculty of Stanford University Space Systems Development Program in Northern California to educate individuals who have interest in satellite technology. The CanSat objective is to collect information and data from the environment. Such data includes air-pressure, temperature, humidity and location data etc. Small cameras can also be installed onto the CanSat to allow images to be capture for further use. Each year, CanSat competitions are held and many participants from over the world joined. During these competitions held, the retrieval of the CanSat hardware have been prove to be tedious as the CanSat is easily sway by strong winds and unforeseen weather conditions. In year 2001, a new objective has been added to the competition which requires participants to retrieve their CanSat hardware after launched. This report will document the method adopted, the “Fly-Back” CanSat. While the CanSat is launched, a parafoils are often deployed to reduce the descending speed of the hardware. This is to allow longer air-borne time for the sensors installed on the CanSat to collect data and also to reduce hardware damage. With the appropriate parafoils attached, an autonomous landing system algorithm can be used to steer the CanSat to a designated landing area for retrieval. Finally, the report will conclude with the test results, analysis and recommendations for future development. In the process of the developing the CanSat prototype, many challenges and problems were encountered. However, with the assistant and ideas provided by the staffs and professors in Nanyang Technological University (NTU), many of these problems and challenges are tackled. Bachelor of Engineering 2014-04-29T02:12:36Z 2014-04-29T02:12:36Z 2014 2014 Final Year Project (FYP) http://hdl.handle.net/10356/59275 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
Koh, Jian Cheng
CanSat, satellite in a soda can
description This report documents the development of a CanSat from scratch to a working prototype. The first CanSat project is initiated in 1999 named, A Rocket Launch for International Student Satellites (ARLISS). It is a collaborative effort with faculty of Stanford University Space Systems Development Program in Northern California to educate individuals who have interest in satellite technology. The CanSat objective is to collect information and data from the environment. Such data includes air-pressure, temperature, humidity and location data etc. Small cameras can also be installed onto the CanSat to allow images to be capture for further use. Each year, CanSat competitions are held and many participants from over the world joined. During these competitions held, the retrieval of the CanSat hardware have been prove to be tedious as the CanSat is easily sway by strong winds and unforeseen weather conditions. In year 2001, a new objective has been added to the competition which requires participants to retrieve their CanSat hardware after launched. This report will document the method adopted, the “Fly-Back” CanSat. While the CanSat is launched, a parafoils are often deployed to reduce the descending speed of the hardware. This is to allow longer air-borne time for the sensors installed on the CanSat to collect data and also to reduce hardware damage. With the appropriate parafoils attached, an autonomous landing system algorithm can be used to steer the CanSat to a designated landing area for retrieval. Finally, the report will conclude with the test results, analysis and recommendations for future development. In the process of the developing the CanSat prototype, many challenges and problems were encountered. However, with the assistant and ideas provided by the staffs and professors in Nanyang Technological University (NTU), many of these problems and challenges are tackled.
author2 Ling Keck Voon
author_facet Ling Keck Voon
Koh, Jian Cheng
format Final Year Project
author Koh, Jian Cheng
author_sort Koh, Jian Cheng
title CanSat, satellite in a soda can
title_short CanSat, satellite in a soda can
title_full CanSat, satellite in a soda can
title_fullStr CanSat, satellite in a soda can
title_full_unstemmed CanSat, satellite in a soda can
title_sort cansat, satellite in a soda can
publishDate 2014
url http://hdl.handle.net/10356/59275
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