408 pgs, 2007,AIAA
ISBN 978-1563479274

Applied Mathematics In Integrated Navigation Systems presents mathematical methods for combining an on-board navigation solution (position, velocity, and attitude), and independent navigation data (aides-to-navigation) to form an integrated navigation system. The first part of the book covers the basic elements of mathematics, kinematics, equations describing navigation systems/sensors and their error models, aides to navigation, and Kalman filtering. Detailed derivations are presented and examples are given. The second part of the book presents case studies that apply the elements to real-world projects.

TABLE OF CONTENTS

1. Mathematical Prelimiaries
2. Coordinate Systems and Transformations
3. Earth Models
4. Terrestrial Navigation
5. Navigation Sensor Models
6. Navigation Aids
7. Kalman Filtering
8. Strap-Down Inertial Sensor Laboroatory Calibration
9. Flight Test Evaluations
10. Inertial Navigation System Ground Alignment
11. Integration via Kalman Filtering: Global Positioning
12. In-Motion Alignment
13. Integrated Differential Global Positioning System/Dead-Reckoning Navigation
14. Summary