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INS/CNS/GNSS Integrated Navigation Technology.

By: Quan, Wei.
Contributor(s): Li, Jianli | Gong, Xiaolin.
Material type: TextTextSeries: eBooks on Demand.Publisher: Berlin : Springer Berlin Heidelberg, 2015Description: 1 online resource (381 p.).ISBN: 9783662451595.Subject(s): Astronautics | Computer engineering | Computer simulation | Engineering | Geographical information systemsGenre/Form: Electronic books.Additional physical formats: Print version:: INS/CNS/GNSS Integrated Navigation TechnologyDDC classification: 003.3 | 620 | 621.3 | 629.1 Online resources: Click here to view this ebook.
Contents:
""Preface""; ""Brief Introductions""; ""Contents""; ""Chapter 1 Introduction""; ""1.1 The History of INS/CNS/GNSS Navigation""; ""1.2 The Current Status of INS/CNS/GNSS Navigation Development""; ""1.2.1 INS/GNSS Navigation""; ""1.2.2 INS/CNS Navigation""; ""1.2.3 INS/CNS/GNSS Navigation""; ""References""; ""Chapter 2 Principle of INS/CNS/GNSS Navigation System""; ""2.1 Introduction""; ""2.2 Coordinate Frames and Earth Reference Model Commonly Used in Navigation""; ""2.2.1 The Coordinate Frames Used in Navigation""; ""2.2.2 The Conversion of Coordinate Systems""
""2.2.3 Earth Reference Model""""2.3 Inertial Navigation System""; ""2.3.1 Work Principle of Inertial Navigation System""; ""2.3.2 SINS System Error Equation and Error Propagation Characteristics""; ""2.4 Satellite Navigation System""; ""2.4.1 Operating Principle of Satellite Navigation System""; ""2.4.2 Analysis of Error Characteristics for Satellite Navigation System""; ""2.5 Celestial Navigation System""; ""2.5.1 Autonomous Celestial Positioning Principle""; ""2.5.2 Celestial Attitude Determination Principle""; ""2.5.3 Star Sensor in CNS and Analysis of Its Error Characteristics""
""2.6 Chapter Conclusion""""References""; ""Chapter 3 Filters in Navigation System""; ""3.1 Introduction""; ""3.2 Kalman Filter""; ""3.3 Extended Kalman Filter""; ""3.3.1 Mathematical Description of Stochastic Nonlinear System""; ""3.3.2 Discrete Extended Kalman Filter""; ""3.4 Unscented Kalman Filter""; ""3.5 Particle Filter""; ""3.6 Unscented Particle Filter (UPF)""; ""3.7 Predictive Filtering""; ""3.8 Federated Filter""; ""3.8.1 Structure of Federated Filter""; ""3.8.2 Fusion Algorithm""; ""3.9 Chapter Conclusion""; ""References""
""Chapter 4 Error Modeling, Calibration, and Compensation of Inertial Measurement Unit (IMU)""""4.1 Introduction""; ""4.2 Error Modeling and Compensation of Inertial Sensors""; ""4.2.1 Error Model of Gyroscopes""; ""4.2.2 Scale Factor Error Modeling of Gyroscope""; ""4.2.3 Temperature Error Modeling of Gyroscope""; ""4.3 Design, Error Calibration, and Compensation of Inertial Measurement Units""; ""4.3.1 Design of Inertial Measurement Units""; ""4.3.2 The Optimization Six-Position Hybrid Calibration for SINS""
""4.3.3 Integrated Calibration Method for RLG IMU Using a Hybrid Analytic/Kalman Filter Approach""""4.3.4 Temperature Error Modeling of IMU Based on Neural Network""; ""4.4 High Dynamic Strapdown Inertial Algorithm""; ""4.4.1 Error Analysis and Gyro Biases Calibration of Analytic Coarse Alignment for Airborne POS""; ""4.4.2 Conical Motion Analysis and Evaluation Criteria for Conical Error Compensation Algorithm""; ""4.4.3 An Improved Single-Subsample Rotating Vector Attitude Algorithm""; ""4.5 Chapter Conclusion""; ""References""
""Chapter 5 Star Map Processing Algorithm of Star Sensor and Autonomous Celestial Navigation""
Summary: This book not only introduces the principles of INS, CNS and GNSS, the related filters and semi-physical simulation, but also systematically discusses the key technologies needed for integrated navigations of INS/GNSS, INS/CNS, and INS/CNS/GNSS, respectively. INS/CNS/GNSS integrated navigation technology has established itself as an effective tool for precise positioning navigation, which can make full use of the complementary characteristics of different navigation sub-systems and greatly improve the accuracy and reliability of the integrated navigation system. The book offers a valuable ref
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QA76.9.C65 (Browse shelf) http://uttyler.eblib.com/patron/FullRecord.aspx?p=1966128 Available EBL1966128

""Preface""; ""Brief Introductions""; ""Contents""; ""Chapter 1 Introduction""; ""1.1 The History of INS/CNS/GNSS Navigation""; ""1.2 The Current Status of INS/CNS/GNSS Navigation Development""; ""1.2.1 INS/GNSS Navigation""; ""1.2.2 INS/CNS Navigation""; ""1.2.3 INS/CNS/GNSS Navigation""; ""References""; ""Chapter 2 Principle of INS/CNS/GNSS Navigation System""; ""2.1 Introduction""; ""2.2 Coordinate Frames and Earth Reference Model Commonly Used in Navigation""; ""2.2.1 The Coordinate Frames Used in Navigation""; ""2.2.2 The Conversion of Coordinate Systems""

""2.2.3 Earth Reference Model""""2.3 Inertial Navigation System""; ""2.3.1 Work Principle of Inertial Navigation System""; ""2.3.2 SINS System Error Equation and Error Propagation Characteristics""; ""2.4 Satellite Navigation System""; ""2.4.1 Operating Principle of Satellite Navigation System""; ""2.4.2 Analysis of Error Characteristics for Satellite Navigation System""; ""2.5 Celestial Navigation System""; ""2.5.1 Autonomous Celestial Positioning Principle""; ""2.5.2 Celestial Attitude Determination Principle""; ""2.5.3 Star Sensor in CNS and Analysis of Its Error Characteristics""

""2.6 Chapter Conclusion""""References""; ""Chapter 3 Filters in Navigation System""; ""3.1 Introduction""; ""3.2 Kalman Filter""; ""3.3 Extended Kalman Filter""; ""3.3.1 Mathematical Description of Stochastic Nonlinear System""; ""3.3.2 Discrete Extended Kalman Filter""; ""3.4 Unscented Kalman Filter""; ""3.5 Particle Filter""; ""3.6 Unscented Particle Filter (UPF)""; ""3.7 Predictive Filtering""; ""3.8 Federated Filter""; ""3.8.1 Structure of Federated Filter""; ""3.8.2 Fusion Algorithm""; ""3.9 Chapter Conclusion""; ""References""

""Chapter 4 Error Modeling, Calibration, and Compensation of Inertial Measurement Unit (IMU)""""4.1 Introduction""; ""4.2 Error Modeling and Compensation of Inertial Sensors""; ""4.2.1 Error Model of Gyroscopes""; ""4.2.2 Scale Factor Error Modeling of Gyroscope""; ""4.2.3 Temperature Error Modeling of Gyroscope""; ""4.3 Design, Error Calibration, and Compensation of Inertial Measurement Units""; ""4.3.1 Design of Inertial Measurement Units""; ""4.3.2 The Optimization Six-Position Hybrid Calibration for SINS""

""4.3.3 Integrated Calibration Method for RLG IMU Using a Hybrid Analytic/Kalman Filter Approach""""4.3.4 Temperature Error Modeling of IMU Based on Neural Network""; ""4.4 High Dynamic Strapdown Inertial Algorithm""; ""4.4.1 Error Analysis and Gyro Biases Calibration of Analytic Coarse Alignment for Airborne POS""; ""4.4.2 Conical Motion Analysis and Evaluation Criteria for Conical Error Compensation Algorithm""; ""4.4.3 An Improved Single-Subsample Rotating Vector Attitude Algorithm""; ""4.5 Chapter Conclusion""; ""References""

""Chapter 5 Star Map Processing Algorithm of Star Sensor and Autonomous Celestial Navigation""

This book not only introduces the principles of INS, CNS and GNSS, the related filters and semi-physical simulation, but also systematically discusses the key technologies needed for integrated navigations of INS/GNSS, INS/CNS, and INS/CNS/GNSS, respectively. INS/CNS/GNSS integrated navigation technology has established itself as an effective tool for precise positioning navigation, which can make full use of the complementary characteristics of different navigation sub-systems and greatly improve the accuracy and reliability of the integrated navigation system. The book offers a valuable ref

Description based upon print version of record.

Author notes provided by Syndetics

<p>QUAN Wei: H-index 7<br> <br> Main publications list:<br> 1. Quan Wei, Fang Jiancheng etc. Hybrid simulation system study of SINS/CNS integrated navigation, IEEE A&E Systems Magazine, 2008, 23(2):17~24.<br> 2. Quan Wei, Fang Jiancheng. A star recognition method based on the adaptive ant colony algorithm for star sensors, Sensors, 2010, 10(3):1955~1966.<br> 3. Quan Wei, Fang Jiancheng, Zhang Weina. A method of optimization for the distorted model of star map based on improved genetic algorithm, Aerospace Science and Technology, 2011, 15(2):103~107.<br> 4. Quan Wei, Xu Liang, Fang Jiancheng. A New Star Pattern Recognition Algorithm based on Improved Hausdorff Distance, IEEE Transactions on AES, In press.<br> 5. Zhang Weina, Quan Wei, Guo Lei. Blurred Star Image Processing for Star Sensor in Dynamic Condition, Sensors, In press.<br> 6. Wang Ziliang, Quan Wei. An All-sky autonomous star map identification algorithm, IEEE A&E Systems Magazine, 2004, 19:10~14.<br> 7. Quan Wei, Zhang Weina. Restoration of motion-blurred star image based on wiener filter, 2011 International Conference on Intelligent Computation Technology and Automation, 2011,3 Vol.II, 691-694<br> 8. Quan Wei, Fang Jiancheng, Guo Lei. An adaptive segmented information fusion method for the attitude determination of nano-spacecrafts, Proceedings of SPIE -Seventh International Symposium on Instrumentation and Control Technology, 2008, 7129:2G<br> 9. Quan Wei, Fang Jiancheng. An adaptive federated filter algorithm based on improved GA and its application, Proceedings of SPIE - Signal Analysis, Measurement Theory, Photo-Electronic Technology, and Artificial Intelligence, 2006, 6357:5C<br> 10. Quan Wei, Fang Jiancheng. Hardware in-the-loop simulation of celestial navigation system, Collection of Technical Papers - AIAA Modeling and Simulation Technologies Conference, 2005, 426-429<br> <br> Research Interest:<br> 1.INS/CNS, INS/CNS/GNSS integrated navigation system technology for airplane or missile.<br> 2.Gyro/Star sensor, Gyro/Celestial sensor/Magnetometer multi-sensors integrated attitude determination system technology.<br> 3.Star sensor system technology based on CMOS APS.<br> 4.Star map processing technology including denoising, distort correcting, centroiding, recognizing, etc.<br> 5.Advanced filtering method based on intelligent algorithm.<br> 6.Deep space exploration payload technology.<br> 7.Atom magnetometer and atom spin gyro technology.</p>

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