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报告编号NASA/TM-2001-211246, L-18125, NAS 1.15:211246
来源IDNTRS_Document_ID: 20020021655
An Approach to Simulation of Extreme Conditions for a Planetary Lander
Queen, Eric M.; Striepe, Scott A.; Powell, Richard W.
英文摘要A "Monte Carlo-like" design analysis tool is developed and applied to an aeromaneuvering Mars entry vehicle. This tool provides realistic but challenging design cases using many fewer cases than a full Monte Carlo analysis. The problem of random input variables that are provided a priori (as opposed to being drawn from a given distribution) is addressed and a solution is found that shows prospects for future improvement.
英文关键词COMPUTERIZED SIMULATION MONTE CARLO METHOD AEROMANEUVERING MARS LANDING DESIGN ANALYSIS ROBUSTNESS (MATHEMATICS) RANDOM VARIABLES SUPERSONICS DEPLOYMENT PARACHUTES TRAJECTORIES
出版年2001
报告类型Technical Report
语种英语
国家美国
URLhttp://hdl.handle.net/2060/20020021655
资源类型科技报告
条目标识符http://119.78.100.177/qdio/handle/2XILL650/259287
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Queen, Eric M.,Striepe, Scott A.,Powell, Richard W.. An Approach to Simulation of Extreme Conditions for a Planetary Lander,2001.
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