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Mathematical Modeling of Aerodynamic Space -to - Surface Flight with Trajectory for Avoid Intercepting Process for Safety and Security Issues
Other Computer Science · Submitted 22 Aug 2009
abstract compiled · 2026-09-23 · no language-model review
The authors' main claim Modeling has been created for a Space-to-Surface system defined for an optimal trajectory in terminal phase.
The compiled record
The paper's own sentences, arranged. Each label is drawn from a closed vocabulary; the number beside it is the probability the classifier gave that label. Numbers in the tables are the authors', checked by code. No sentence in this record was written by a model.
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The abstract, sentence by sentence
The research project has been made for mathematical modeling of aerospace system Space-to-Surface for avoid intercepting process by flight objects Surface-to-Air. The research has been completed and created mathematical models which used for research and statistical analysis. In mathematical modeling has been including a few models: Model of atmosphere, Model of speed of sound, Model of flight head in space, Model of flight in atmosphere, Models of navigation and guidance, Model and statistical analysis of approximation of aerodynamic characteristics. Modeling has been created for a Space-to-Surface system defined for an optimal trajectory in terminal phase. The modeling includes models for simulation atmosphere, aerodynamic flight and navigation by an infrared system. The modeling simulation includes statistical analysis of the modeling results.
background contribution method result interpretation main claim
| # | sentence | role | the authors' own work | states the main conclusion | strength |
|---|---|---|---|---|---|
| s0 | The research project has been made for mathematical modeling of aerospace system Space-to-Surface for avoid intercepting process by flight objects Surface-to-Air. | contribution 0.91 | 0.81 | 0.08 | asserted 0.94 |
| s1 | The research has been completed and created mathematical models which used for research and statistical analysis. | contribution 0.89 | 0.89 | 0.12 | asserted 1.00 |
| s2 | In mathematical modeling has been including a few models: Model of atmosphere, Model of speed of sound, Model of flight head in space, Model of flight in atmosphere, Models of navigation and guidance, Model and statistical analysis of approximation of aerodynamic characteristics. | method 0.93 | 0.82 | 0.05 | asserted 1.00 |
| s3 | Modeling has been created for a Space-to-Surface system defined for an optimal trajectory in terminal phase. | contribution 0.56 | 0.88 | 0.21 | asserted 1.00 |
| s4 | The modeling includes models for simulation atmosphere, aerodynamic flight and navigation by an infrared system. | method 0.94 | 0.82 | 0.06 | asserted 1.00 |
| s5 | The modeling simulation includes statistical analysis of the modeling results. | method 0.93 | 0.83 | 0.07 | asserted 1.00 |
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The paper
Original abstract
The research project has been made for mathematical modeling of aerospace system Space-to-Surface for avoid intercepting process by flight objects Surface-to-Air. The research has been completed and created mathematical models which used for research and statistical analysis. In mathematical modeling has been including a few models: Model of atmosphere, Model of speed of sound, Model of flight head in space, Model of flight in atmosphere, Models of navigation and guidance, Model and statistical analysis of approximation of aerodynamic characteristics. Modeling has been created for a Space-to-Surface system defined for an optimal trajectory in terminal phase. The modeling includes models for simulation atmosphere, aerodynamic flight and navigation by an infrared system. The modeling simulation includes statistical analysis of the modeling results.
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How the literature uses it
Papers whose main result relates to this one's
States the same result 2 papers
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Modeling has been created for a Space-to-Surface system defined for an optimal trajectory for targeting in terminal phase.
Modeling of aerodynamic Space-to-Surface flight with optimal trajectory for targeting · 0.88
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Modeling has been created for a Space-to-Surface system defined for an optimal trajectory for targeting in terminal phase with avoids an intercepting process.
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