2H Singularity-Free Momentum Generation with Non-Redundant Single Gimbaled Control Moment Gyroscopes

Abstract

Two objectives dominate consideration of control moment gyroscopes (CMGs) for spacecraft maneuvers: High torque (equivalently momentum) and singularity-free operations. This paper adds to the significant body of research towards these two goals utilizing a minimal 3-CMG array to provide 646% singularity-free momentum performance increase spherically, compared to the ubiquitous pyramid arrangement skewed at 54.730. Spherical 1H (1 CMGs-worth momentum) singularity free momentum is established with birectional 1H and 2H in the third direction in a baseline configuration. Lastly, momentum space reshaping is shown via mixed skew angles. These claims are demonstrated analytically, then heuristically, and finally validated experimentally.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 2006
Accession Number
ADA601121

Entities

People

  • Brij Agrawal
  • Jae J. Kim
  • Timothy A. Sands

Organizations

  • Naval Postgraduate School

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Abstracts
  • Air Force
  • Angular Momentum
  • Control Systems Engineering
  • Demographic Cohorts
  • Electronic Mail
  • Engineering
  • Engineers
  • Geometry
  • Gimbals
  • Gyroscopes
  • Maneuvers
  • Momentum
  • Saturation
  • Simulators
  • Spacecraft
  • Trajectories

Fields of Study

  • Physics

Readers

  • Adaptive Control and Estimation with Uncertainty in Dynamic Systems.
  • Electromagnetic Wave Scattering and Antenna Radiation Engineering
  • Robotics and Automation.

Technology Areas

  • Space
  • Space - Spacecraft Maneuvers