This presentation details work performed during the Fall 2011 term in the Research Controls and Dynamics Branch at NASA Dryden Flight Research Center. Included is a study on a possible landing footprint algorithm, with direct application to the HTV-2. Also discussed is work in support of the MIPCC effort, which includes optimal trajectory solutions for the F-15A Streak Eagle aircraft and theoretical performance of an F-15A with a MIPCC propulsion system.
Implementation of a Landing Footprint Algorithm for the HTV-2 and Trajectory Simulations
2012-04-30
Sonstige
Keine Angabe
Englisch
Rapid generation of landing footprint based on geometry-predicted trajectory
Online Contents | 2017
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|Rapid generation of landing footprint based on geometry-predicted trajectory
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