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Taschenbuch. Condizione: Neu. Magnetometer Aided Inertial Navigation System | MODELING AND SIMULATION OF A NAVIGATION SYSTEM WITH AN IMU AND A MAGNETOMETER | U¿ur Kayasal | Taschenbuch | 168 S. | Englisch | 2009 | LAP LAMBERT Academic Publishing | EAN 9783838317403 | Verantwortliche Person für die EU: OmniScriptum GmbH & Co. KG, Bahnhofstr. 28, 66111 Saarbrücken, info[at]akademikerverlag[dot]de | Anbieter: preigu.…

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Taschenbuch. Condizione: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -In this book, the integration of a MEMS based inertial measurement unit and a three axis solid state magnetometer are studied. It is a fact that unaided inertial navigation systems, especially low cost MEMS based navigation systems have a divergent behavior. Nowadays, many navigation systems use GPS aiding to improve the performance, but GPS may not be applicable in some cases. Also, GPS provides the position and velocity reference whereas the attitude information is extracted through estimation filters. An alternative reference source is a three axis magnetometer, which provides direct attitude measurements. In this study, error propagation equations of an inertial navigation system are derived; measurement equations of magnetometer for Kalman filtering are v developed; the unique method to self align the MEMS navigation system is developed. In the motion estimation, the performance of the developed algorithms are compared using a GPS aided system and magnetometer aided system. Some experiments are conducted for self alignment algorithms. 168 pp. Englisch.…

Condizione: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. In this book, the integration of a MEMS based inertial measurement unit and a three axis solid state magnetometer are studied. It is a fact that unaided inertial navigation systems, especially low cost MEMS based navigation systems have a divergent behavior. …

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.…

Taschenbuch. Condizione: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - In this book, the integration of a MEMS based inertial measurement unit and a three axis solid state magnetometer are studied. It is a fact that unaided inertial navigation systems, especially low cost MEMS based navigation systems have a divergent behavior. Nowadays, many navigation systems use GPS aiding to improve the performance, but GPS may not be applicable in some cases. Also, GPS provides the position and velocity reference whereas the attitude information is extracted through estimation filters. An alternative reference source is a three axis magnetometer, which provides direct attitude measurements. In this study, error propagation equations of an inertial navigation system are derived; measurement equations of magnetometer for Kalman filtering are v developed; the unique method to self align the MEMS navigation system is developed. In the motion estimation, the performance of the developed algorithms are compared using a GPS aided system and magnetometer aided system. Some experiments are conducted for self alignment algorithms.…

Taschenbuch. Condizione: Neu. This item is printed on demand - Print on Demand Titel. Neuware -In this book, the integration of a MEMS based inertial measurement unit and a three axis solid state magnetometer are studied. It is a fact that unaided inertial navigation systems, especially low cost MEMS based navigation systems have a divergent behavior. Nowadays, many navigation systems use GPS aiding to improve the performance, but GPS may not be applicable in some cases. Also, GPS provides the position and velocity reference whereas the attitude information is extracted through estimation filters. An alternative reference source is a three axis magnetometer, which provides direct attitude measurements. In this study, error propagation equations of an inertial navigation system are derived; measurement equations of magnetometer for Kalman filtering are v developed; the unique method to self align the MEMS navigation system is developed. In the motion estimation, the performance of the developed algorithms are compared using a GPS aided system and magnetometer aided system. Some experiments are conducted for self alignment algorithms.VDM Verlag, Dudweiler Landstraße 99, 66123 Saarbrücken 168 pp. Englisch.…

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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.…

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.…

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.…

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. …