DEVELOPMENT OF PICOSATELLITE MECHANICAL PLATFORM AND COMMUNICATION PROTOCOL

<p align="justify"> <br /> <br /> Picosatellite is a type of satellite with small size and maximum mass of 1 kg. With a small mass, picosatellite has advantages because it can be built at a low cost and also needs much cheaper launching cost. Common applications of picosa...

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Main Author: REYNALD (NIM : 13214091), BRIAN
Format: Final Project
Language:Indonesia
Online Access:https://digilib.itb.ac.id/gdl/view/26152
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Institution: Institut Teknologi Bandung
Language: Indonesia
id id-itb.:26152
spelling id-itb.:261522018-06-25T08:09:15ZDEVELOPMENT OF PICOSATELLITE MECHANICAL PLATFORM AND COMMUNICATION PROTOCOL REYNALD (NIM : 13214091), BRIAN Indonesia Final Project INSTITUT TEKNOLOGI BANDUNG https://digilib.itb.ac.id/gdl/view/26152 <p align="justify"> <br /> <br /> Picosatellite is a type of satellite with small size and maximum mass of 1 kg. With a small mass, picosatellite has advantages because it can be built at a low cost and also needs much cheaper launching cost. Common applications of picosatellite are for remote sensing and as the relay station for amateur radio communication. <br /> <br /> In developed countries, the role of universities and research institutes in the development of picosatellites is very significant. Unfortunately in Indonesia, the role of universities and research institutes in the development of picosatellite is still low. Here, the picosatellite simulator was developed as an effort to motivate the public about the importance of satellite technology. <br /> <br /> The objective of picosatellite simulator is to demonstrate the attitude control processes of the actual picosatellite system in this case by using reaction wheels. In order to better represent the environment in space, the picosatellite simulator is equipped with air bearing suspension system and Helmholtz coils. <br /> <br /> The reaction wheels serve to regulate the attitude of the picosatellite simulator through rotation that produces angular momentum. By modifying the angular momentum, the center of mass of the picosatellite simulator can change directions perpendicular to the rotation axis. <br /> <br /> The air suspension system aims to produce minimum frictional force conditions. The Helmholtz coils serve to generate a magnetic field to mimic the effects of the earth's magnetic field as a reference for the attitude control. <br /> <br /> In order to communicate with picosatellite simulator, a communication protocol that connects the user to picosatellite simulator is required. The data exchange is protected with a security system so that the system is not easily hacked by unauthorized parties. The selected wireless communication is Bluetooth which include AES encryption-decryption, authentication, anti-replay attack, and data integrity. Wireless communication has a role in transmitting input from the user in form of control mode and manual mode data of the attitude angle. Data logging of the picosatellite simulator attitude angle is also facilitated by this wireless communication. <br /> <p align="justify"> text
institution Institut Teknologi Bandung
building Institut Teknologi Bandung Library
continent Asia
country Indonesia
Indonesia
content_provider Institut Teknologi Bandung
collection Digital ITB
language Indonesia
description <p align="justify"> <br /> <br /> Picosatellite is a type of satellite with small size and maximum mass of 1 kg. With a small mass, picosatellite has advantages because it can be built at a low cost and also needs much cheaper launching cost. Common applications of picosatellite are for remote sensing and as the relay station for amateur radio communication. <br /> <br /> In developed countries, the role of universities and research institutes in the development of picosatellites is very significant. Unfortunately in Indonesia, the role of universities and research institutes in the development of picosatellite is still low. Here, the picosatellite simulator was developed as an effort to motivate the public about the importance of satellite technology. <br /> <br /> The objective of picosatellite simulator is to demonstrate the attitude control processes of the actual picosatellite system in this case by using reaction wheels. In order to better represent the environment in space, the picosatellite simulator is equipped with air bearing suspension system and Helmholtz coils. <br /> <br /> The reaction wheels serve to regulate the attitude of the picosatellite simulator through rotation that produces angular momentum. By modifying the angular momentum, the center of mass of the picosatellite simulator can change directions perpendicular to the rotation axis. <br /> <br /> The air suspension system aims to produce minimum frictional force conditions. The Helmholtz coils serve to generate a magnetic field to mimic the effects of the earth's magnetic field as a reference for the attitude control. <br /> <br /> In order to communicate with picosatellite simulator, a communication protocol that connects the user to picosatellite simulator is required. The data exchange is protected with a security system so that the system is not easily hacked by unauthorized parties. The selected wireless communication is Bluetooth which include AES encryption-decryption, authentication, anti-replay attack, and data integrity. Wireless communication has a role in transmitting input from the user in form of control mode and manual mode data of the attitude angle. Data logging of the picosatellite simulator attitude angle is also facilitated by this wireless communication. <br /> <p align="justify">
format Final Project
author REYNALD (NIM : 13214091), BRIAN
spellingShingle REYNALD (NIM : 13214091), BRIAN
DEVELOPMENT OF PICOSATELLITE MECHANICAL PLATFORM AND COMMUNICATION PROTOCOL
author_facet REYNALD (NIM : 13214091), BRIAN
author_sort REYNALD (NIM : 13214091), BRIAN
title DEVELOPMENT OF PICOSATELLITE MECHANICAL PLATFORM AND COMMUNICATION PROTOCOL
title_short DEVELOPMENT OF PICOSATELLITE MECHANICAL PLATFORM AND COMMUNICATION PROTOCOL
title_full DEVELOPMENT OF PICOSATELLITE MECHANICAL PLATFORM AND COMMUNICATION PROTOCOL
title_fullStr DEVELOPMENT OF PICOSATELLITE MECHANICAL PLATFORM AND COMMUNICATION PROTOCOL
title_full_unstemmed DEVELOPMENT OF PICOSATELLITE MECHANICAL PLATFORM AND COMMUNICATION PROTOCOL
title_sort development of picosatellite mechanical platform and communication protocol
url https://digilib.itb.ac.id/gdl/view/26152
_version_ 1822921800452931584