A presentation of the basic theory and the possible functions of a digital computer program which mathematically simulates the motions of an earth satellite, permitting cheap, accurate predictions of orbital changes for years ahead. Its applications include evaluating systems which stress satellite longevity and orbital stability, estimating drag characteristics of unknown satellites, and improving or refining a new model atmosphere.
This report is part of the RAND Corporation research memorandum series. The Research Memorandum was a product of the RAND Corporation from 1948 to 1973 that represented working papers meant to report current results of RAND research to appropriate audiences.
Permission is given to duplicate this electronic document for personal use only, as long as it is unaltered and complete. Copies may not be duplicated for commercial purposes. Unauthorized posting of RAND PDFs to a non-RAND Web site is prohibited. RAND PDFs are protected under copyright law. For information on reprint and linking permissions, please visit the RAND Permissions page.
The RAND Corporation 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.