Some Results of Adding Solar Radiation Pressure Force to the Restricted Three-Body Problem

Abstract

This work explores the generation of bounded orbits in the Elliptic Restricted Three-Body Problem *ER3BP), and some of the results of adding the solar radiation pressure force to the ER3BP are presented. The focus is limited to the equilibrium points defined in the Sun-Earth ER3BP. (These equilibrium points are also referred to as libration points or Lagrange points.) The addition of solar radiation pressure to the gravitational and centrifugal force structure alters the locations and conditions for linear stability of the equilibrium points in the Sun Earth ER3BP. Solar radiation pressure also consequently affects the spacecraft orbits computed near these points. One equilibrium point in this three-body system is located between the Sun and the Earth; orbits near this point are the primary focus for the study of solar effects on the terrestrial environment and are therefore the orbits considered here.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1991
Accession Number
ADA241397

Entities

People

  • Steven C. Gordon

Organizations

  • United States Air Force Academy

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Air Force
  • Artificial Satellites
  • Astronautics
  • Celestial Mechanics
  • Differential Equations
  • Equations Of Motion
  • Radiation
  • Radiation Pressure
  • Solar Radiation
  • Solar Wind
  • Spacecraft
  • Spacecraft Orbits
  • Three Dimensional
  • Two Dimensional
  • United States
  • Variational Equations
  • Warning Systems

Readers

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

Technology Areas

  • Space
  • Space - Orbital Debris