Mathematical Modeling of Aerodynamic Space -to - Surface Flight with Trajectory for Avoid Intercepting Process

Simple item page
dc.creatorGornev, Serge
dc.date2006-03-29
dc.date.accessioned2026-07-07T12:54:53Z
dc.date.available2026-07-07T12:54:53Z
dc.descriptionModeling has been created for a Space-to-Surface system defined for an optimal trajectory for targeting in terminal phase with avoids an intercepting process. The modeling includes models for simulation atmosphere, speed of sound, aerodynamic flight and navigation by an infrared system. The modeling and simulation includes statistical analysis of the modeling results.
dc.identifierhttps://arxiv.org/abs/cs/0603113
dc.identifierhttp://arxiv.org/abs/cs/0603113
dc.identifier.urihttp://salesiana.dossiersoluciones.com/handle/123456789/224093
dc.subjectOther Computer Science
dc.titleMathematical Modeling of Aerodynamic Space -to - Surface Flight with Trajectory for Avoid Intercepting Process
dc.typetext

Files

Collections

arXiv