Articoli correlati a Transfer Alignment for Inertial Navigation Systems
Informazioni sull'autore
Dr. U¿ur Kayasal received the B.Sc degree in Mechanical Engineering in 2004, B.Sc degree in Aerospace Engineering in 2005, M.Sc degree in Mechanical Engineering in 2007 and Ph.D degree in Mechanical Engineering in 2012 from Middle East Technical University. His main research areas are inertial navigation systems and estimation theory.
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Transfer alignment is the process of initialization of a guided munition¿s inertial navigation system with the aid of the carrier platform¿s navigation system. One important problem in transfer alignment is the attitude uncertainty of lever arm between munition¿s and carrier¿s navigation systems. In order to have a rapid transfer alignment, attitude data should be included in transfer alignment with proper handling of lever arm uncertainty. Modeling and compensation of vibration induced inertial sensor errors should also be done in rapid transfer alignment The purpose of this book is to compensate the errors arising from the dynamics of the platform, lever arm, mechanical vibration effects and inertial sensor error amplification, thus designing a transfer alignment algorithm under real environment conditions. The algorithm design begins with observability analysis, which is not done in detail for transfer alignment in literature. In order to make proper compensations, characterization and modeling of vibration and lever arm environment is done for the helicopter. Also, vibration based errors of MEMS based inertial sensors are experimentally shown.
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Transfer Alignment for Inertial Navigation Systems
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Condizione: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Kayasal UgurDr. Ugur Kayasal received the B.Sc degree in Mechanical Engineering in 2004, B.Sc degree in Aerospace Engineering in 2005, M.Sc degree in Mechanical Engineering in 2007 and Ph.D degree in Mechanical Engineering in 2012 fr. Codice articolo 518430448
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Transfer Alignment for Inertial Navigation Systems
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Transfer Alignment for Inertial Navigation Systems
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Scholars' Press Jan 2014, 2014
ISBN 10: 3639705491
ISBN 13: 9783639705492
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Taschenbuch. Condizione: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -Transfer alignment is the process of initialization of a guided munition¿s inertial navigation system with the aid of the carrier platform¿s navigation system. One important problem in transfer alignment is the attitude uncertainty of lever arm between munition¿s and carrier¿s navigation systems. In order to have a rapid transfer alignment, attitude data should be included in transfer alignment with proper handling of lever arm uncertainty. Modeling and compensation of vibration induced inertial sensor errors should also be done in rapid transfer alignment The purpose of this book is to compensate the errors arising from the dynamics of the platform, lever arm, mechanical vibration effects and inertial sensor error amplification, thus designing a transfer alignment algorithm under real environment conditions. The algorithm design begins with observability analysis, which is not done in detail for transfer alignment in literature. In order to make proper compensations, characterization and modeling of vibration and lever arm environment is done for the helicopter. Also, vibration based errors of MEMS based inertial sensors are experimentally shown. 240 pp. Englisch. Codice articolo 9783639705492
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Transfer Alignment for Inertial Navigation Systems
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Taschenbuch. Condizione: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - Transfer alignment is the process of initialization of a guided munition's inertial navigation system with the aid of the carrier platform's navigation system. One important problem in transfer alignment is the attitude uncertainty of lever arm between munition's and carrier's navigation systems. In order to have a rapid transfer alignment, attitude data should be included in transfer alignment with proper handling of lever arm uncertainty. Modeling and compensation of vibration induced inertial sensor errors should also be done in rapid transfer alignment The purpose of this book is to compensate the errors arising from the dynamics of the platform, lever arm, mechanical vibration effects and inertial sensor error amplification, thus designing a transfer alignment algorithm under real environment conditions. The algorithm design begins with observability analysis, which is not done in detail for transfer alignment in literature. In order to make proper compensations, characterization and modeling of vibration and lever arm environment is done for the helicopter. Also, vibration based errors of MEMS based inertial sensors are experimentally shown. Codice articolo 9783639705492
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Transfer Alignment for Inertial Navigation Systems
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Scholars' Press Jan 2014, 2014
ISBN 10: 3639705491
ISBN 13: 9783639705492
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Da: buchversandmimpf2000, Emtmannsberg, BAYE, Germania
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Taschenbuch. Condizione: Neu. This item is printed on demand - Print on Demand Titel. Neuware -Transfer alignment is the process of initialization of a guided munition's inertial navigation system with the aid of the carrier platform's navigation system. One important problem in transfer alignment is the attitude uncertainty of lever arm between munition's and carrier's navigation systems. In order to have a rapid transfer alignment, attitude data should be included in transfer alignment with proper handling of lever arm uncertainty. Modeling and compensation of vibration induced inertial sensor errors should also be done in rapid transfer alignment The purpose of this book is to compensate the errors arising from the dynamics of the platform, lever arm, mechanical vibration effects and inertial sensor error amplification, thus designing a transfer alignment algorithm under real environment conditions. The algorithm design begins with observability analysis, which is not done in detail for transfer alignment in literature. In order to make proper compensations, characterization and modeling of vibration and lever arm environment is done for the helicopter. Also, vibration based errors of MEMS based inertial sensors are experimentally shown.OmniScriptum SRL, Str. Armeneasca 28/1, office 1, 2012 Chisinau 240 pp. Englisch. Codice articolo 9783639705492
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Taschenbuch. Condizione: Neu. Transfer Alignment for Inertial Navigation Systems | U¿ur Kayasal | Taschenbuch | Englisch | 2014 | Scholars' Press | EAN 9783639705492 | Verantwortliche Person für die EU: preigu GmbH & Co. KG, Lengericher Landstr. 19, 49078 Osnabrück, mail[at]preigu[dot]de | Anbieter: preigu Print on Demand. Codice articolo 120699994
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