ERROR ANALYSIS OF SINGLE AND TWO-FORCE FIELD SPACECRAFT ORBITS,

Abstract

It is the purpose of astronautical error analysis to express mathematically the effect of errors or deliberate changes in velocity on the orbital elements of either transfer orbit or terminal orbit. (Author)

Document Details

Document Type
Technical Report
Publication Date
Sep 22, 1958
Accession Number
AD0673134

Entities

People

  • K. A. Ehricke

Organizations

  • General Dynamics

Tags

DTIC Thesaurus Topics

  • Error Analysis
  • Errors
  • Orbital Elements
  • Orbits
  • Spacecraft
  • Spacecraft Orbits
  • Terminals
  • Transfer Orbits

Fields of Study

  • Physics

Readers

  • Space Exploration and Orbital Mechanics.
  • Theoretical Analysis.

Technology Areas

  • Space
  • Space - Orbital Debris
  • Space - Spacecraft Maneuvers