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  • © 2021

General Relativity for Planetary Navigation

  • Explores General Relativity from a space navigation perspective
  • Provides a linear progression from theory to experimental results in planetary spacecraft navigation
  • Includes detailed explanations of mathematical operations involved in spaceflight, starting from first principles

Part of the book series: SpringerBriefs in Space Development (BRIEFSSPACE)

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Table of contents (4 chapters)

  1. Front Matter

    Pages i-vi
  2. Einstein Field Equations

    • James Miller, Connie J. Weeks
    Pages 1-30
  3. Schwarzschild Solution for Spherical Symmetry

    • James Miller, Connie J. Weeks
    Pages 31-46
  4. Comparison of Numerical Integration and Analytic Solutions

    • James Miller, Connie J. Weeks
    Pages 47-74
  5. General Relativity Time Delay Experiment

    • James Miller, Connie J. Weeks
    Pages 75-97
  6. Back Matter

    Pages 99-104

About this book

This brief approaches General Relativity from a planetary navigation perspective, delving into the unconventional mathematical methods required to produce computer software for space missions. It provides a derivation of the Einstein field equations and describes experiments performed on the Near Earth Asteroid Rendezvous mission, spanning General Relativity Theory from the fundamental assumptions to experimental verification.

The software used for planetary missions is derived from mathematics that use matrix notation.  An alternative is to use Einstein summation notation, which enables the mathematics to be presented in a compact form but makes the geometry difficult to understand.  In this book, the relationship of matrix notation to summation notation is shown.  The purpose is to enable the reader to derive the mathematics used in the software in either matrix notation or summation notation. 

This brief is a useful tool for advanced students andyoung professionals embarking on careers in planetary navigation.

Authors and Affiliations

  • Porter Ranch, USA

    James Miller

  • Loyola Marymount University, Northridge, USA

    Connie J. Weeks

About the authors

James Miller worked as the assistant Navigation Team Chief on the Viking Mission to Mars in 1976. In 2000, he received the Mechanics and Control of Flight medal from the AIAA for his design of the navigation system for the first orbiting and landing on the asteroid Eros. Further, he designed a trajectory to leave Earth and orbit the Moon with no propulsive maneuvers. This was the first practical solution of the four-body problem, and it has since been used on the missions Hiten, Genesis, and Grail. 

Bibliographic Information

Buy it now

Buying options

eBook USD 54.99
Price excludes VAT (USA)
  • Available as EPUB and PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book USD 69.99
Price excludes VAT (USA)
  • Compact, lightweight edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info

Tax calculation will be finalised at checkout

Other ways to access