Optimal Kalman Filter Integration Of A Global Positioning System Receiver And An Ln 94 Inertial Navigation System

Download Optimal Kalman Filter Integration Of A Global Positioning System Receiver And An Ln 94 Inertial Navigation System full books in PDF, epub, and Kindle. Read online Optimal Kalman Filter Integration Of A Global Positioning System Receiver And An Ln 94 Inertial Navigation System ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!

Optimal Kalman Filter Integration of a Global Positioning System Receiver and an LN-94 Inertial Navigation System

Author : James L. Hirning
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (639 download)

DOWNLOAD NOW!

Book Synopsis Optimal Kalman Filter Integration of a Global Positioning System Receiver and an LN-94 Inertial Navigation System by : James L. Hirning

Download or read book Optimal Kalman Filter Integration of a Global Positioning System Receiver and an LN-94 Inertial Navigation System written by James L. Hirning and published by . This book was released on 1990 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: This research develops and attempts to implement a Kalman filter integration of a Phase III Global Positioning System (GPS) five-channel receiver and an LN-94 Inertial Navigation System (INS). The GPS provides highly accurate position and velocity information in low dynamic environments. An INS provides position and velocity information with lower accuracy over long periods of time, but it is highly responsive in dynamic maneuvers or at high frequencies. The INS has the added advantage of requiring no signals external to the vehicle to function. The integration of these two systems provide more precise information under a wider variety of situations. A truth model for the INS is verified. A GPS error model is developed and combined with the INS model to provide GPS- aided INS navigation. This model is used to predict baseline performance of all full-ordered filter. Attempts are made to utilize the filter with empirical data. The data is analyzed, and suggestions are made about ways to account for the errors in evidence. Results to date are presented and analyzed. Keywords: Global positioning system, Inertial navigation system, GPS/INS Integration, GPS- aided-INS, Theses.

Optimal Kalman Filter Integration of a Global Positioning System Receiver and an LN-94 Inertial Navigation System

Author : James L. Hirning
Publisher :
ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (639 download)

DOWNLOAD NOW!

Book Synopsis Optimal Kalman Filter Integration of a Global Positioning System Receiver and an LN-94 Inertial Navigation System by : James L. Hirning

Download or read book Optimal Kalman Filter Integration of a Global Positioning System Receiver and an LN-94 Inertial Navigation System written by James L. Hirning and published by . This book was released on 1990 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This research develops and attempts to implement a Kalman filter integration of a Phase III Global Positioning System (GPS) five-channel receiver and an LN-94 Inertial Navigation System (INS). The GPS provides highly accurate position and velocity information in low dynamic environments. An INS provides position and velocity information with lower accuracy over long periods of time, but it is highly responsive in dynamic maneuvers or at high frequencies. The INS has the added advantage of requiring no signals external to the vehicle to function. The integration of these two systems provide more precise information under a wider variety of situations. A truth model for the INS is verified. A GPS error model is developed and combined with the INS model to provide GPS- aided INS navigation. This model is used to predict baseline performance of all full-ordered filter. Attempts are made to utilize the filter with empirical data. The data is analyzed, and suggestions are made about ways to account for the errors in evidence. Results to date are presented and analyzed. Keywords: Global positioning system, Inertial navigation system, GPS/INS Integration, GPS- aided-INS, Theses.

Optimal Kalman Filter Integration of a Global Positioning System Receiver and an LN-94 Intertial Navigation System

Author : James Lawrence Hirning
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (132 download)

DOWNLOAD NOW!

Book Synopsis Optimal Kalman Filter Integration of a Global Positioning System Receiver and an LN-94 Intertial Navigation System by : James Lawrence Hirning

Download or read book Optimal Kalman Filter Integration of a Global Positioning System Receiver and an LN-94 Intertial Navigation System written by James Lawrence Hirning and published by . This book was released on 1990 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Global Positioning Systems, Inertial Navigation, and Integration

Author : Mohinder S. Grewal
Publisher : John Wiley & Sons
ISBN 13 : 0471463868
Total Pages : 415 pages
Book Rating : 4.4/5 (714 download)

DOWNLOAD NOW!

Book Synopsis Global Positioning Systems, Inertial Navigation, and Integration by : Mohinder S. Grewal

Download or read book Global Positioning Systems, Inertial Navigation, and Integration written by Mohinder S. Grewal and published by John Wiley & Sons. This book was released on 2004-04-05 with total page 415 pages. Available in PDF, EPUB and Kindle. Book excerpt: The only comprehensive guide to Kalman filtering and its applications to real-world GPS/INS problems Written by recognized authorities in the field, this book provides engineers, computer scientists, and others with a working familiarity with the theory and contemporary applications of Global Positioning Systems (GPS), Inertial Navigational Systems, and Kalman filters. Throughout, the focus is on solving real-world problems, with an emphasis on the effective use of state-of-the-art integration techniques for those systems, especially the application of Kalman filtering. To that end, the authors explore the various subtleties, common failures, and inherent limitations of the theory as it applies to real-world situations, and provide numerous detailed application examples and practice problems, including GPS-aided INS, modeling of gyros and accelerometers, and WAAS and LAAS. Drawing upon their many years of experience with GPS, INS, and the Kalman filter, the authors present numerous design and implementation techniques not found in other professional references, including original techniques for: * Representing the problem in a mathematical model * Analyzing the performance of the GPS sensor as a function of model parameters * Implementing the mechanization equations in numerically stable algorithms * Assessing computation requirements * Testing the validity of results * Monitoring GPS, INS, and Kalman filter performance in operation In order to enhance comprehension of the subjects covered, the authors have included software in MATLAB, demonstrating the workings of the GPS, INS, and filter algorithms. In addition to showing the Kalman filter in action, the software also demonstrates various practical aspects of finite word length arithmetic and the need for alternative algorithms to preserve result accuracy.

Scientific and Technical Aerospace Reports

Author :
Publisher :
ISBN 13 :
Total Pages : 308 pages
Book Rating : 4.:/5 (3 download)

DOWNLOAD NOW!

Book Synopsis Scientific and Technical Aerospace Reports by :

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1991 with total page 308 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Fundamentals of Inertial Navigation, Satellite-based Positioning and their Integration

Author : Aboelmagd Noureldin
Publisher : Springer Science & Business Media
ISBN 13 : 3642304656
Total Pages : 324 pages
Book Rating : 4.6/5 (423 download)

DOWNLOAD NOW!

Book Synopsis Fundamentals of Inertial Navigation, Satellite-based Positioning and their Integration by : Aboelmagd Noureldin

Download or read book Fundamentals of Inertial Navigation, Satellite-based Positioning and their Integration written by Aboelmagd Noureldin and published by Springer Science & Business Media. This book was released on 2012-10-28 with total page 324 pages. Available in PDF, EPUB and Kindle. Book excerpt: Fundamentals of Inertial Navigation, Satellite-based Positioning and their Integration is an introduction to the field of Integrated Navigation Systems. It serves as an excellent reference for working engineers as well as textbook for beginners and students new to the area. The book is easy to read and understand with minimum background knowledge. The authors explain the derivations in great detail. The intermediate steps are thoroughly explained so that a beginner can easily follow the material. The book shows a step-by-step implementation of navigation algorithms and provides all the necessary details. It provides detailed illustrations for an easy comprehension. The book also demonstrates real field experiments and in-vehicle road test results with professional discussions and analysis. This work is unique in discussing the different INS/GPS integration schemes in an easy to understand and straightforward way. Those schemes include loosely vs tightly coupled, open loop vs closed loop, and many more.

Integrated Navigation and Guidance Systems

Author : Daniel J. Biezad
Publisher : AIAA
ISBN 13 : 9781600860713
Total Pages : 262 pages
Book Rating : 4.8/5 (67 download)

DOWNLOAD NOW!

Book Synopsis Integrated Navigation and Guidance Systems by : Daniel J. Biezad

Download or read book Integrated Navigation and Guidance Systems written by Daniel J. Biezad and published by AIAA. This book was released on 1999 with total page 262 pages. Available in PDF, EPUB and Kindle. Book excerpt: Annotation Beginning with the basic principles of navigation, "Integrated Navigation and Guidance Systems takes a step beyond introductions with a concise look at the flight applications of inertial navigation systems integrated with Global Positioning System (GPS) satellite systems. Written at the senior engineering college level, the textbook takes a tutorial approach, weaving interrelated disciplines together with interactive computer exercises and AINSBOOK software for error analysis and Kalman filter simulation. Get a "technical jump start" with a look at traditional navigation radio aids, inertial guidance systems, and Kalman filters. Launch into GPS applications to navigation, precision approach and landing, attitude control, and air traffic control. More than 100 figures, photos, and tables add to the textbook's value.

The Global Positioning System & Inertial Navigation

Author : Jay A. Farrell
Publisher : McGraw Hill Professional
ISBN 13 : 9780071369442
Total Pages : 360 pages
Book Rating : 4.3/5 (694 download)

DOWNLOAD NOW!

Book Synopsis The Global Positioning System & Inertial Navigation by : Jay A. Farrell

Download or read book The Global Positioning System & Inertial Navigation written by Jay A. Farrell and published by McGraw Hill Professional. This book was released on 1999-01-21 with total page 360 pages. Available in PDF, EPUB and Kindle. Book excerpt: With GPS and INS hardware becoming ever smaller and less expensive, innovative opportunities for commercial navigation systems are everywhereÑand continue to arise. Integrated GPS/INS systems have some real advantages, in terms of output rate, reliability, and accuracy. The Global Positioning System and Inertial Navigation is the first-ever reference to provide engineers and scientists with a detailed, top-to-bottom look at GPS and INS in a single volume. This in-depth text provides navigation system designers comprehensive and accurate coverage of such topics as coordinate frames and transformations, Kalman filtering techniques, navigation system performance analysis, GPS receiver ephemeris and pseudo-range processing, differential GPS, carrier phase processing, and attitude determination. Extensively cross-referenced to the literature on advanced navigation system design, this superb engineering reference is ideal for navigation systems designers, analysts, and project managers.

Global Navigation Satellite Systems, Inertial Navigation, and Integration

Author : Mohinder S. Grewal
Publisher : John Wiley & Sons
ISBN 13 : 1119547830
Total Pages : 610 pages
Book Rating : 4.1/5 (195 download)

DOWNLOAD NOW!

Book Synopsis Global Navigation Satellite Systems, Inertial Navigation, and Integration by : Mohinder S. Grewal

Download or read book Global Navigation Satellite Systems, Inertial Navigation, and Integration written by Mohinder S. Grewal and published by John Wiley & Sons. This book was released on 2020-01-22 with total page 610 pages. Available in PDF, EPUB and Kindle. Book excerpt: Covers significant changes in GPS/INS technology, and includes new material on GPS, GNSSs including GPS, Glonass, Galileo, BeiDou, QZSS, and IRNSS/NAViC, and MATLAB programs on square root information filtering (SRIF) This book provides readers with solutions to real-world problems associated with global navigation satellite systems, inertial navigation, and integration. It presents readers with numerous detailed examples and practice problems, including GNSS-aided INS, modeling of gyros and accelerometers, and SBAS and GBAS. This revised fourth edition adds new material on GPS III and RAIM. It also provides updated information on low cost sensors such as MEMS, as well as GLONASS, Galileo, BeiDou, QZSS, and IRNSS/NAViC, and QZSS. Revisions also include added material on the more numerically stable square-root information filter (SRIF) with MATLAB programs and examples from GNSS system state filters such as ensemble time filter with square-root covariance filter (SRCF) of Bierman and Thornton and SigmaRho filter. Global Navigation Satellite Systems, Inertial Navigation, and Integration, 4th Edition provides: Updates on the significant upgrades in existing GNSS systems, and on other systems currently under advanced development Expanded coverage of basic principles of antenna design, and practical antenna design solutions More information on basic principles of receiver design, and an update of the foundations for code and carrier acquisition and tracking within a GNSS receiver Examples demonstrating independence of Kalman filtering from probability density functions of error sources beyond their means and covariances New coverage of inertial navigation to cover recent technology developments and the mathematical models and methods used in its implementation Wider coverage of GNSS/INS integration, including derivation of a unified GNSS/INS integration model, its MATLAB implementations, and performance evaluation under simulated dynamic conditions Global Navigation Satellite Systems, Inertial Navigation, and Integration, Fourth Edition is intended for people who need a working knowledge of Global Navigation Satellite Systems (GNSS), Inertial Navigation Systems (INS), and the Kalman filtering models and methods used in their integration.

Proceedings of the IEEE 1992 National Aerospace and Electronics Conference, NAECON 1992

Author :
Publisher :
ISBN 13 :
Total Pages : 462 pages
Book Rating : 4.:/5 (318 download)

DOWNLOAD NOW!

Book Synopsis Proceedings of the IEEE 1992 National Aerospace and Electronics Conference, NAECON 1992 by :

Download or read book Proceedings of the IEEE 1992 National Aerospace and Electronics Conference, NAECON 1992 written by and published by . This book was released on 1992 with total page 462 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA SP.

Author :
Publisher :
ISBN 13 :
Total Pages : 654 pages
Book Rating : 4.:/5 (319 download)

DOWNLOAD NOW!

Book Synopsis NASA SP. by :

Download or read book NASA SP. written by and published by . This book was released on 1992 with total page 654 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Integration of Differential GPS and Inertial Navigation Using a Complementary Kalman Filter

Author : Carl W. Marquis
Publisher :
ISBN 13 :
Total Pages : 101 pages
Book Rating : 4.:/5 (64 download)

DOWNLOAD NOW!

Book Synopsis Integration of Differential GPS and Inertial Navigation Using a Complementary Kalman Filter by : Carl W. Marquis

Download or read book Integration of Differential GPS and Inertial Navigation Using a Complementary Kalman Filter written by Carl W. Marquis and published by . This book was released on 1993 with total page 101 pages. Available in PDF, EPUB and Kindle. Book excerpt: Precise navigation with high update rates is essential for automatic landing of an unmanned aircraft. Individual sensors currently available - INS, AHRS, GPS, LORAN, etc. - cannot meet both requirements. The most accurate navigation sensor available today is the Global Positioning System or GPS. However, GPS updates only come once per second. INS, being an on-board sensor, is available as often as necessary. Unfortunately, it is subject to the Schuler cycle, biases, noise floor, and cross-axis sensitivity. In order to design and verify a precise, high update rate navigation system, a working model of Differential GPS has been developed including all of the major GPS error sources - clock differences, atmospherics, selective availability and receiver noise. A standard INS system was also modeled, complete with the inaccuracies mentioned. The outputs of these two sensors - inertial acceleration and pseudoranges - can be optimally blended with a complementary Kalman filter for positioning. Eventually, in the discrete case, the high update rate and high precision required for autoland can be achieved.

Integration of Differential GPS and Inertial Navigation Using a Complementary Kalman Filter

Author : Carl W. Marquis
Publisher :
ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (64 download)

DOWNLOAD NOW!

Book Synopsis Integration of Differential GPS and Inertial Navigation Using a Complementary Kalman Filter by : Carl W. Marquis

Download or read book Integration of Differential GPS and Inertial Navigation Using a Complementary Kalman Filter written by Carl W. Marquis and published by . This book was released on 1993 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: Precise navigation with high update rates is essential for automatic landing of an unmanned aircraft. Individual sensors currently available - INS, AHRS, GPS, LORAN, etc. - cannot meet both requirements. The most accurate navigation sensor available today is the Global Positioning System or GPS. However, GPS updates only come once per second. INS, being an on-board sensor, is available as often as necessary. Unfortunately, it is subject to the Schuler cycle, biases, noise floor, and cross-axis sensitivity. In order to design and verify a precise, high update rate navigation system, a working model of Differential GPS has been developed including all of the major GPS error sources - clock differences, atmospherics, selective availability and receiver noise. A standard INS system was also modeled, complete with the inaccuracies mentioned. The outputs of these two sensors - inertial acceleration and pseudoranges - can be optimally blended with a complementary Kalman filter for positioning. Eventually, in the discrete case, the high update rate and high precision required for autoland can be achieved.

Integration of the Global Positioning System with an Inertial Navigation System

Author : Derek Marvel
Publisher :
ISBN 13 :
Total Pages : 37 pages
Book Rating : 4.:/5 (455 download)

DOWNLOAD NOW!

Book Synopsis Integration of the Global Positioning System with an Inertial Navigation System by : Derek Marvel

Download or read book Integration of the Global Positioning System with an Inertial Navigation System written by Derek Marvel and published by . This book was released on 1998 with total page 37 pages. Available in PDF, EPUB and Kindle. Book excerpt: Navigation is the determination of the position and velocity of a moving vehicle. Navigation systems used to measure this state vector can be one of two types, either positioning or dead-reckoning. Positioning systems, such as the Global Positioning System (GPS) measure the state vector without regard to the path traveled by the vehicle in the past. On the other hand, dead-reckoning navigation systems, such as the Inertial Navigation System (INS) determine the state vector from a continuous series of measurements relative to an initial position. By integrating the unique and complementary characteristics of each system into one integrated INS/GPS system, accuracies as well as additional benefits can be achieved even though unattainable by either system independently. The optimal method of integrating these two systems is through the use of a Kalman filter. This mathematical technique is used for computing the best estimate of the state of a process which varies with time. Approaches to this filtering can either be centralized in a main filter or federated, where filtering is done at individual sensors. This theory can then be applied to real world scenarios, whether it be an aircraft during flight, an aircraft during precision approach landings, or the failure detection and isolation of a GPS signal.

The Evaluation of Kalman Filter Designs for Multisensor Integrated Navigation Systems

Author : Joseph A. D'Appolito
Publisher :
ISBN 13 :
Total Pages : 206 pages
Book Rating : 4.F/5 ( download)

DOWNLOAD NOW!

Book Synopsis The Evaluation of Kalman Filter Designs for Multisensor Integrated Navigation Systems by : Joseph A. D'Appolito

Download or read book The Evaluation of Kalman Filter Designs for Multisensor Integrated Navigation Systems written by Joseph A. D'Appolito and published by . This book was released on 1971 with total page 206 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Kalman Filter Based Integrated Air Data/GPS Navigation System

Author : Taner Mutlu
Publisher : LAP Lambert Academic Publishing
ISBN 13 : 9783844301755
Total Pages : 148 pages
Book Rating : 4.3/5 (17 download)

DOWNLOAD NOW!

Book Synopsis Kalman Filter Based Integrated Air Data/GPS Navigation System by : Taner Mutlu

Download or read book Kalman Filter Based Integrated Air Data/GPS Navigation System written by Taner Mutlu and published by LAP Lambert Academic Publishing. This book was released on 2012 with total page 148 pages. Available in PDF, EPUB and Kindle. Book excerpt: This monograph is focused on the improvement of the modern navigation systems. In aeronautics high precision is very essential. Global Positioning System (GPS) has revolutionized the navigation systems. In this study GPS position measurements obtained from a GPS receiver, are improved using Kalman Filter based Satellite Distances method. The GPS receiver provides us with both available satellite positions and the position of the receiver. Using this information in the Kalman Filter a better position compared to the GPS receiver alone was aimed. In the monograph the integration of two navigation systems ADS and GPS was aimed. ADS is a widely used navigation system which measures static and total air pressure and the air temperature. ADS has high sampling frequency and poor accuracy, on the other hand, GPS has high accuracy compared to ADS but lower sampling frequency. Kalman Filter is used to integrate and minimize the errors of the two navigation systems. By this integration a navigation system with high sampling frequency and high accuracy is aimed. Another object is to calculate the wind speed with high accuracy, which is actually the error of Air Speed measured by the ADS.

Aeronautical Engineering

Author :
Publisher :
ISBN 13 :
Total Pages : 712 pages
Book Rating : 4.F/5 ( download)

DOWNLOAD NOW!

Book Synopsis Aeronautical Engineering by :

Download or read book Aeronautical Engineering written by and published by . This book was released on 1993 with total page 712 pages. Available in PDF, EPUB and Kindle. Book excerpt: A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)