Gradiometer-Aided Inertial Navigation.

Abstract

The purpose of the study is to develop a technique for combining gradiometer and inertial navigation system (INS) outputs that minimizes the navigation and gravity rms errors, and to determine the gradiometer accuracy needed for typical aircraft and marine navigation and gravity-mapping applications.

Document Details

Document Type
Technical Report
Publication Date
Apr 07, 1975
Accession Number
ADA013274

Entities

People

  • Warren G. Heller

Organizations

  • TASC, Inc

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Accuracy
  • Aircrafts
  • Errors
  • Gradiometers
  • Guidance
  • Inertial Navigation
  • Inertial Navigation Systems
  • Marine Navigation
  • Navigation
  • Navigational Equipment

Readers

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