Rogers, a consultant to the Department of Defense and NASA, explains elements of integrated navigation systems and describes applications in this text/reference for those directly involved with the design, integration, testing, and evaluation of navigation systems. For the purposes of the discussion, the integration of onboard navigation and independent navigation data is accomplished with Kalman filter algorithms. The first section of the book covers basic mathematics, kinematics, equations for describing navigation systems/sensors and their error models, aids-to-navigation, and Kalman filtering. Detailed derivations and examples are presented, and chapter problems are included. Chapters in the second section describe applications in areas such as inertial navigating system ground alignment, in-motion alignment, and attitude-determination and estimation. With this third edition, software for exercises can be downloaded from a web site. Readers are assumed to have background in mathematics, including calculus. Annotation ©2007 Book News, Inc., Portland, OR (booknews.com)
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Robert M. Rogers received his degrees in aerospace engineering from the University of Florida and is an Associate Fellow of the American Institute of Aeronautics and Astronautics. As sole proprietor of Rogers Engineering & Associates, Dr. Roberts performs research development, systems analysis, test and evaluation, and teaching for the Department of Defense and the National Aeronautics and Space Administration in integrated navigation systems.
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