Planetary atmosphere representation for Monte-Carlo simulation of aerospace vehicle trajectories

Details Planetary atmosphere representation for Monte-Carlo simulation of aerospace vehicle trajectories Planetary atmosphere representation for Monte-Carlo simulation of aerospace vehicle trajectories

Sep 1990

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1990stia...9116724d&link_type=abstract

AIAA, Flight Simulation Technologies Conference and Exhibit, Dayton, OH, Sept. 17-19, 1990. 22 p.

Computer Science

Performance

Aerospace Vehicles, Monte Carlo Method, Planetary Atmospheres, Spacecraft Trajectories, Aeroassist, Flight Tests, Vertical Distribution

Scientific paper

Methods of simulating large scale random atmospheric variations are examined for use in Monte Carlo simulations of hypervelocity vehicles. Random density, temperature, and pressure variations have a significant impact on the performance of such vehicles. Methods for generating random atmosphere profiles are described and compared in the context of a Monte Carlo simulation of the Aeroassist Flight Experiment (AFE). It is seen that these techniques result in statistically significant differences in key simulation point statistics.

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