Observer's Position and Velocity Determination Using Satellite Doppler Measurements

Abstract

Existing navigation techniques using satellite doppler shift measurements are sensitive to observer velocity errors. A model is developed for determining the position and velocity of the observer with the result that the navigation process will be independent of external velocity source error. The position and velocity determination will be feasible provided that precision reference oscillators with instabilities of about 2 parts in 10 to the 12th power be used in the satellite and the navigator's equipment. Relativistic and tropospheric effects must be accounted for in the model. The feasibility also depends on the satellite velocity error being less than 0.05 meter per second.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1968
Accession Number
AD0393899

Entities

People

  • E. W. Hix

Organizations

  • Johns Hopkins University

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Artificial Satellites
  • Classification
  • Computational Science
  • Computer Programming
  • Doppler Effect
  • Frequency
  • Government Procurement
  • Inertial Navigation
  • Inertial Navigation Systems
  • Measurement
  • National Security
  • Navigation
  • Navigational Equipment
  • Oscillators
  • Physics Laboratories
  • Security
  • United States

Fields of Study

  • Physics

Readers

  • Atmospheric Remote Sensing.
  • Fluid Dynamics.
  • Inertial Navigation Systems.

Technology Areas

  • Space
  • Space - Orbital Debris