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The subject of integrated navigation systems covered in this
book is designed for those directly involved with the design,
integration, and test and evaluation of navigation systems. It is
assumed that the reader has a background in mathematics, including
calculus. Integrated navigation systems are the combination of an
onboard navigation solution (position, velocity, and attitude) and
independent navigation data (aids to navigation) to update or
correct navigation solutions. In this book, this combination is
accomplished with Kalman filter algorithms.
Elements of basic mathematics, kinematics, equations describing
navigation systems/sensors and their error models, aids to
navigation, and Kalman filtering are developed. Detailed
derivations are presented and examples are given to aid in the
understanding of these elements of integrated navigation systems.
Problems are included to expand the application of the materials
presented.
The third edition includes additional background material,
exercises and software. The added material includes: development of
general form for Earth's gravitational potential with
simplification to an ellipsoid model; development of satellite
orbital equations for position and velocity and the impact of
non-spherical earth gravitation on satellite orbital parameters;
and illustrations in the development of derivative-free Kalman
filters including the Unscented and Divided Difference filter
forms. Additional exercises are included that expand and supplement
the material in the text and demonstrate properties of the Kalman
filter. Additional software is included in this edition for
simulating random processes and derivative-free filter
implementations.
This edition provides a more complete foundation for addressing the
different aspects of integrated navigation systems.
| Product Code |
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| ISBN: 9781563479274 Robert Rogers |
Hardback 2006 |
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£69.00
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