Perturbations of a gravity gradient stabilization system

Richard H. Frick

ResearchPublished 1965

An investigation of several sources of perturbation on the performance of a gravity gradient stabilization system, including micro-meteoroid impact, solar radiation pressure, station-keeping propulsion, orbital eccentricity, and on-board rotating machinery. Formulas are developed that determine the magnitude of pitch, roll, and yaw perturbations from each of these effects. These perturbations do not neccessarily rule out gravity gradient stabilization, but their magnitudes for a given vehicle configuration should be considered in the light of mission requirements.

Document Details

  • Availability: Web Only
  • Year: 1965
  • Pages: 72
  • Document Number: RM-4679-ARPA

Citation

Chicago Manual of Style

Frick, Richard H., Perturbations of a gravity gradient stabilization system. Santa Monica, CA: RAND Corporation, 1965. https://www.rand.org/pubs/research_memoranda/RM4679.html.
BibTeX RIS

This publication is part of the RAND research memorandum series. The research memorandum series, a product of RAND from 1948 to 1973, included working papers meant to report current results of RAND research to appropriate audiences.

This document and trademark(s) contained herein are protected by law. This representation of RAND intellectual property is provided for noncommercial use only. Unauthorized posting of this publication online is prohibited; linking directly to this product page is encouraged. Permission is required from RAND to reproduce, or reuse in another form, any of its research documents for commercial purposes. For information on reprint and reuse permissions, please visit www.rand.org/pubs/permissions.

RAND is a nonprofit institution that helps improve policy and decisionmaking through research and analysis. RAND's publications do not necessarily reflect the opinions of its research clients and sponsors.