SATELLITE RESONANCE WITH LONGITUDE-DEPENDENT GRAVITY. 2. EFFECTS INVOLVING THE ECCENTRICITY,

Abstract

For a satellite in a nominally circular orbit at arbitrary inclination whose mean motion is commensurable with the Earth's rotation, the dependence of gravity on longitude leads to a resonant variation in eccentricity as well as the long-period oscillation in longitude. Provided forces capable of precessing perigee are present, it is shown that the change in eccentricity for a satellite captured in librational resonance is not secular but periodic. There are corresponding resonance effects for a satellite in a nominally equatorial but eccentric orbit. Here the commensurability condition is that the longitudes of the apses shall be nearly repetitive relative to the rotating Earth. There will be a long-period oscillation in longitude which can take the form of either a libration (trapped) or a circulation (free), and there will also be an oscillation of the orbital plane having the same period as the precession of perigee relative to inertial space. (Author)

Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1967
Accession Number
AD0665961

Entities

People

  • R. R. Allen

Organizations

  • Royal Aircraft Establishment

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Artificial Satellites
  • Circular Orbits
  • Eccentric Orbits
  • Eccentricity
  • Longitude
  • Motion
  • Orbits
  • Oscillation
  • Precession
  • Resonance
  • Rotation

Readers

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

Technology Areas

  • Space
  • Space - Orbital Debris