A Parametric Analysis of Endoatmospheric Low-Earth-Orbit Maintenance

Abstract

With the advent of long term low Earth-orbiting satellites comes the requirement to maintain a specified orbital radial band. Optimal control theory suggests that periodic thrusting is more efficient than forced Keplerian motion in orbital maintenance through the use of Primer vectoring. This thesis examined the efficiency of fixed-angle transverse thrusting as an alternative to Primer vectoring. Numerical analysis shows that a thrust angle of 65-70 degrees is feasible for radial band control for a wide range of parameters. Fuel usage can be minimized through the proper selection of radial bandwidth, thruster size, and thrust angle. This thesis shows that forced Keplerian motion is always superior to fixed-angle transverse thrusting from a fuel usage standpoint, and hence that thrust vectoring must be utilized

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1993
Accession Number
ADA265868

Entities

People

  • Mark S. Wilsey

Organizations

  • Naval Postgraduate School

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Altitude
  • Angular Momentum
  • Apogees
  • Artificial Satellites
  • Astronautics
  • Atmospheric Density
  • Computer Programs
  • Computers
  • Equations Of Motion
  • Low Earth Orbits
  • Orbits
  • Satellite Orbits
  • Space Stations
  • Spacecraft
  • Spacecraft Orbits
  • United States
  • United States Naval Academy

Fields of Study

  • Physics

Readers

  • Control Systems Engineering.
  • Space Exploration and Orbital Mechanics.
  • Systems Analysis and Design

Technology Areas

  • Space
  • Space - Hall-Effect Thruster
  • Space - Orbital Debris
  • Space - Spacecraft Maneuvers