Description

Book Synopsis
Formulation for Observed and Computed Values of Deep Space Network Data Types for Navigation documents the formation of the Regres of the Orbit Determination Program (ODP) of the Jet Propulsion Laboratory (JPL). Program Regres calculates the computed values of observed quantities (e.g.

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.

Deep Space Network Data Types 3 JPL DeepSpace

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A Hardback by Theodore D. Moyer

15 in stock


    View other formats and editions of Deep Space Network Data Types 3 JPL DeepSpace by Theodore D. Moyer

    Publisher: John Wiley & Sons Inc
    Publication Date: 14/02/2003
    ISBN13: 9780471445357, 978-0471445357
    ISBN10: 0471445355

    Description

    Book Synopsis
    Formulation for Observed and Computed Values of Deep Space Network Data Types for Navigation documents the formation of the Regres of the Orbit Determination Program (ODP) of the Jet Propulsion Laboratory (JPL). Program Regres calculates the computed values of observed quantities (e.g.

    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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