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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.
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- ÉditeurLAP Lambert Academic Publishing
- Date d'édition2010
- ISBN 10 3838313127
- ISBN 13 9783838313122
- ReliureBroché
- Nombre de pages112
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Design of an Attitude Determination Subsystem for Nanosatellites: A cheap satellite navigation system
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(2010)
ISBN 10 : 3838313127
ISBN 13 : 9783838313122
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Description du livre Etat : New. N° de réf. du vendeur ABLIING23Apr0316110080694
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Design of an Attitude Determination Subsystem for Nanosatellites
Edité par
LAP Lambert Academic Publishing
(2010)
ISBN 10 : 3838313127
ISBN 13 : 9783838313122
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Description du livre Etat : New. PRINT ON DEMAND Book; New; Fast Shipping from the UK. No. book. N° de réf. du vendeur ria9783838313122_lsuk
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Design of an Attitude Determination Subsystem for Nanosatellites
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(2010)
ISBN 10 : 3838313127
ISBN 13 : 9783838313122
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Description du livre Taschenbuch. Etat : Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -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. 112 pp. Englisch. N° de réf. du vendeur 9783838313122
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Design of an Attitude Determination Subsystem for Nanosatellites A cheap satellite navigation system
Edité par
LAP Lambert Academic Publishing
(2010)
ISBN 10 : 3838313127
ISBN 13 : 9783838313122
Neuf
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Description du livre PAP. Etat : New. New Book. Shipped from UK. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000. N° de réf. du vendeur L0-9783838313122
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Design of an Attitude Determination Subsystem for Nanosatellites : A cheap satellite navigation system
Edité par
LAP LAMBERT Academic Publishing
(2010)
ISBN 10 : 3838313127
ISBN 13 : 9783838313122
Neuf
Taschenbuch
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Evaluation vendeur
Description du livre Taschenbuch. Etat : Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - 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. N° de réf. du vendeur 9783838313122
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EUR 49
Autre devise
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Design of an Attitude Determination Subsystem for Nanosatellites A cheap satellite navigation system
Edité par
LAP Lambert Academic Publishing
(2010)
ISBN 10 : 3838313127
ISBN 13 : 9783838313122
Neuf
PAP
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Description du livre PAP. Etat : New. New Book. Delivered from our UK warehouse in 4 to 14 business days. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000. N° de réf. du vendeur L0-9783838313122
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Design of an Attitude Determination Subsystem for Nanosatellites
Edité par
LAP LAMBERT Academic Publishing
(2010)
ISBN 10 : 3838313127
ISBN 13 : 9783838313122
Neuf
Couverture souple
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Description du livre Etat : New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: NASLIN MathieuStudent 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.The purpose of this study is to. N° de réf. du vendeur 5412007
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Design of an Attitude Determination Subsystem for Nanosatellites: A cheap satellite navigation system
Edité par
LAP Lambert Academic Publishing
(2010)
ISBN 10 : 3838313127
ISBN 13 : 9783838313122
Neuf
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Description du livre N° de réf. du vendeur STOCK12782585
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