NASA NTRS · 19770000420
Optimizing simulated trajectories
Abstract
General-purpose rigid-body six-degrees-of-freedom program is used to solve wide variety of atmospheric flight mechanics and orbital transfer problems. Written for analysis of powered or unpowered vehicles operation near rotating oblate planet, typical applications include: guidance and flight-control system simulation and analysis, loads and dispersion-type analysis.
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Brauer, G. L., Habeger, A. R., Stevenson, R.. 1978-03-01. Optimizing simulated trajectories. https://ntrs.nasa.gov/citations/19770000420
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