Multi-Tethered Space-Based Interferometers: Particle System Model

Abstract

Dynamics models are presented for a class of space-based interferometers comprised of multiple component bodies, interconnected in various arrangements, by low-mass flexible tethers of variable length. The tethered constellations are to perform coordinated rotational scanning accompanied by baseline dimensional changes, as well as spin axis realignments and spin-up/spin-down maneuvers. The mechanical idealization is a system of N point masses interconnected by massless tethers of variable length. Both extensible and inextensible tethers are considered. Expressions for system angular and linear momenta are developed. The unrestricted nonlinear motion equations are derived via Lagranges equations. Rheonomic constraints are introduced to allow prescribed motion of any degrees of freedom, and the associated physical forces are determined. The linearized equations of motion are obtained for the steady rotation of a system with extensible tethers of constant unstrained length.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Sep 14, 2001
Accession Number
ADA395110

Entities

People

  • Stephen S. Gates

Organizations

  • United States Naval Research Laboratory

Tags

Communities of Interest

  • Advanced Electronics
  • Air Platforms
  • Space

DTIC Thesaurus Topics

  • Angular Momentum
  • Coefficients
  • Computational Science
  • Constitutive Equations
  • Differential Equations
  • Dynamics
  • Equations
  • Equations Of Motion
  • Interferometers
  • Linear Momentum
  • Maneuvers
  • Mechanics
  • Momentum
  • Particles
  • Rotation
  • Space Based
  • Steady State

Fields of Study

  • Physics

Readers

  • Control Systems Engineering.
  • Fault Tolerant Diagnosis of Black and White Balloon Isolation Tests Using ¥.
  • Structural Dynamics.

Technology Areas

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