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

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      Book details

      Publisher John Wiley & Sons Inc
      Published 14 February 2003
      ISBN-13 9780471445357
      978-0471445357
      ISBN-10 0471445355
      Also in:
      Theoretical and mathematical astronomy Electronics and communications engineering Space science

      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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