Gauge Freedom in the N-body Problem of Celestial Mechanics

Abstract

Whenever a standard system of six planetary equations(in the Lagrange, Delaunay, or other form) is employed, the trajectory resides on a 9(N-1)-dimensional submanifold of the 12(N-1)-dimensional space spanned by the orbital elements and their time derivatives. The freedom in choosing this submanifold reveals an internal symmetry inherent in the description of the trajectory by orbital elements. This freedom is analogous to the gauge invariance of electrodynamics. In traditional derivations of the planetary equations this freedom is removed by hand through the introduction of the Lagrange constraint, either explicitly (in the variation-of-parameters method) or implicitly (in the Hamilton-Jacobi approach). This constraint imposes the condition that the orbital elements osculate the trajectory, i.e., that both the instantaneous position and velocity be fit by a Keplerian ellipse (or hyperbola). Imposition of an supplementary constraint different from that of Lagrange (but compatible with the equations of motion) would alter the mathematical form of the planetary equations without affecting the physical trajectory.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jul 07, 2003
Accession Number
ADA423238

Entities

People

  • Michael Efroimsky
  • Peter Goldreich

Organizations

  • United States Naval Observatory

Tags

Communities of Interest

  • Air Platforms
  • Space

DTIC Thesaurus Topics

  • Angular Momentum
  • Astronomy
  • Celestial Mechanics
  • Coordinate Systems
  • Differential Equations
  • Equations
  • Equations Of Motion
  • Grids
  • Invariance
  • Mechanics
  • Momentum
  • N Body Problem
  • Orbital Elements
  • Orbits
  • Perturbations
  • Symmetry
  • Trajectories

Fields of Study

  • Physics

Readers

  • Calculus or Mathematical Analysis
  • Space Exploration and Orbital Mechanics.

Technology Areas

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