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An introduction to orbit dynamics and its application to satellite-based earth monitoring systemsThe long term behavior of satellites is studied at a level of complexity suitable for the initial planning phases of earth monitoring missions. First-order perturbation theory is used to describe in detail the basic orbit dynamics of satellite motion around the earth and relative to the sun. Surface coverage capabilities of satellite orbits are examined. Several examples of simulated observation and monitoring missions are given to illustrate representative applications of the theory. The examples stress the need for devising ways of maximizing total mission output in order to make the best possible use of the resultant data base as input to those large-scale, long-term earth monitoring activities which can best justify the use of satellite systems.
Document ID
19780004170
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Reference Publication (RP)
Authors
Brooks, D. R.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
November 1, 1977
Subject Category
Astrodynamics
Report/Patent Number
NASA-RP-1009
L-11710
Report Number: NASA-RP-1009
Report Number: L-11710
Accession Number
78N12113
Funding Number(s)
PROJECT: RTOP 683-75-33-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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