Orbital Perturbations Due to Attitude Libration of an Arbitrary Rigid Body Moving in a Central Newtonian Field.

Abstract

Interaction between attitude libration and orbital motion of a rigid body moving in a central Newtonian field is studied. Linearized equation of motion in the neighborhood of a circular orbit are presented, and gravity-gradient stability analysis is extended to include effects of the above interaction. The phenomenon of pitch resonance is explained in terms of this interaction. An average solution of the coupled orbital-attitude motion in the plane is presented. (Author)

Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1970
Accession Number
AD0878076

Entities

People

  • Srinivas N. Mohan

Organizations

  • Stanford University

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Circular Orbits
  • Equations
  • Mathematical Analysis
  • Mathematics
  • Motion
  • Numerical Analysis
  • Orbits
  • Perturbations
  • Resonance

Fields of Study

  • Physics

Readers

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

Technology Areas

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