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Design of an Attitude Determination Subsystem for Nanosatellites
A cheap satellite navigation system
Taschenbuch von Mathieu Naslin
Sprache: Englisch

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Beschreibung
The purpose of this study is to design and analyze the accuracy of an attitude determination subsystem for a satellite of the CubeSat class by using low cost sensors. A 3-axis attitude determination platform has been designed with emphasis on the use of low cost, off the shelf sensors. The principles of observation and the description of the acquisition method are explained. Computation of the attitude has been tested using the Three Axis Attitude Determination scheme (TRIAD). A test bench has been designed to be able to perform accurate rotation measurements. Easily feasible test procedures have been used to test the precision of each component of the acquisition and computing scheme. This study has been especially focused on providing the general platform for the algorithm. Later studies will be necessary to make the subsystem more robust and accurate enough to be used in a real mission. The different ways to improve the system and its accuracy are discussed both for specific items and the entire sensing module.
The purpose of this study is to design and analyze the accuracy of an attitude determination subsystem for a satellite of the CubeSat class by using low cost sensors. A 3-axis attitude determination platform has been designed with emphasis on the use of low cost, off the shelf sensors. The principles of observation and the description of the acquisition method are explained. Computation of the attitude has been tested using the Three Axis Attitude Determination scheme (TRIAD). A test bench has been designed to be able to perform accurate rotation measurements. Easily feasible test procedures have been used to test the precision of each component of the acquisition and computing scheme. This study has been especially focused on providing the general platform for the algorithm. Later studies will be necessary to make the subsystem more robust and accurate enough to be used in a real mission. The different ways to improve the system and its accuracy are discussed both for specific items and the entire sensing module.
Über den Autor
Student in Aerospace engineering at Embry-Riddle Aeronautical University, I defended this thesis for my Masters degree in 2009. Dr Bogdan Udrea helped me a lot to accomplish this task.
Details
Erscheinungsjahr: 2010
Fachbereich: Raumfahrttechnik
Genre: Mathematik, Medizin, Naturwissenschaften, Technik
Rubrik: Naturwissenschaften & Technik
Medium: Taschenbuch
Inhalt: 112 S.
ISBN-13: 9783838313122
ISBN-10: 3838313127
Sprache: Englisch
Ausstattung / Beilage: Paperback
Einband: Kartoniert / Broschiert
Autor: Naslin, Mathieu
Hersteller: LAP LAMBERT Academic Publishing
Verantwortliche Person für die EU: LAP Lambert Academic Publishing, Brivibas Gatve 197, ?-1039 Riga, customerservice@vdm-vsg.de
Maße: 220 x 150 x 7 mm
Von/Mit: Mathieu Naslin
Erscheinungsdatum: 25.03.2010
Gewicht: 0,185 kg
Artikel-ID: 101228879
Über den Autor
Student in Aerospace engineering at Embry-Riddle Aeronautical University, I defended this thesis for my Masters degree in 2009. Dr Bogdan Udrea helped me a lot to accomplish this task.
Details
Erscheinungsjahr: 2010
Fachbereich: Raumfahrttechnik
Genre: Mathematik, Medizin, Naturwissenschaften, Technik
Rubrik: Naturwissenschaften & Technik
Medium: Taschenbuch
Inhalt: 112 S.
ISBN-13: 9783838313122
ISBN-10: 3838313127
Sprache: Englisch
Ausstattung / Beilage: Paperback
Einband: Kartoniert / Broschiert
Autor: Naslin, Mathieu
Hersteller: LAP LAMBERT Academic Publishing
Verantwortliche Person für die EU: LAP Lambert Academic Publishing, Brivibas Gatve 197, ?-1039 Riga, customerservice@vdm-vsg.de
Maße: 220 x 150 x 7 mm
Von/Mit: Mathieu Naslin
Erscheinungsdatum: 25.03.2010
Gewicht: 0,185 kg
Artikel-ID: 101228879
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