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LAUNCH WINDOW ANALYSIS USING THE IGOS PROGRAM
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English
Abstract
The launch window processor in the IGOS program, a sophisticated multipurpose space mission planning program, is presented. The specific problem of launch window analysis using the velocity matching model, that is for missions having fixed impulse upper stage motors with a target mission orbit plane, is discussed in some detail.
Authors
Citation
REYNOLDS, R. and CALABIA, M., "LAUNCH WINDOW ANALYSIS USING THE IGOS PROGRAM," SAE Technical Paper 861648, 1986, https://doi.org/10.4271/861648.Also In
References
- Chu S.T. Lang T.J. Wynn B.E. “A Velocity Matching Technique for Three Dimensional Orbit Transfer in Conceptual Mission Design” Journal of Astornautical Sciences XXVI 4 343 68