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Cover image for Formulation for observed and computed values of Deep Space Network data types for navigation
Title:
Formulation for observed and computed values of Deep Space Network data types for navigation
Personal Author:
Series:
Deep-space communications and navigation series
Publication Information:
Hoboken, N.J. : Wiley-Interscience, 2003
ISBN:
9780471445357

Available:*

Library
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Call Number
Material Type
Item Category 1
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30000010062011 TL4030 M69 2003 Open Access Book Book
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Summary

Summary

A valuable reference for students and professionals in the field of deep space navigation

Drawing on fundamental principles and practices developed during decades of deep space exploration at the California Institute of Technology's Jet Propulsion Laboratory (JPL), this book documents the formation of program Regres of JPL's Orbit Determination Program (ODP). Program Regres calculates the computed values of observed quantities (e.g., Doppler and range observables) obtained at the tracking stations of the Deep Space Network, and also calculates media corrections for the computed values of the observable and partial derivatives of the computed values of the observables with respect to the solve-for-parameter vector-q. The ODP or any other program which uses its formulation can be used to navigate a spacecraft anywhere in the solar system.

A publication of the JPL Deep Space Communications and Navigation System Center of Excellence (DESCANSO), Formulation for Observed and Computed Values of Deep Space Network Data Types for Navigation is an invaluable resource for graduate students of celestial mechanics or astrodynamics because it:
* features the expertise of today's top scientists
* places the entire program Regres formulation in an easy-to-access resource
* describes technology which will be used in the next generation of navigation software currently under development

The Deep Space Communications and Navigation Series is authored by scientists and engineers with extensive experience in astronautics, communications, and related fields. It lays the foundation for innovation in the areas of deep space navigation and communications by conveying state-of-the-art knowledge in key technologies.


Author Notes

THEODORE D. MOYER, now retired, is a former senior engineer in the Navigation and Mission Design Section of the California Institute of Technology's Jet Propulsion Laboratory.


Table of Contents

Foreword
Preface
Acknowledgments
Introduction
Time Scales and Time Differences
Planetary Ephemeris, Small-Body Ephemeris, and Satellite Ephemerides
Spacecraft Ephemeris and Partials File
Geocentric Space-Fixed Position, Velocity, and Acceleration Vectors of Tracking Station
Space-Fixed Position, Velocity, and Acceleration Vectors of a Landed Spacecraft Relative to Center of Mass of Planet, Planetary System, or the Moon
Algorithms for Computing ET-TAI
Light-Time Solution
Angles
Media and Antenna Corrections
Calculation of Precision Light Times and Quasar Delays
Partial Derivatives of Precision Light Times and Quasar Delays
Observables
References
Acronyms
Index
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