Mars Science Laboratory simulations for entry, descent, and landing

被引:74
作者
Striepe, SA [1 ]
Way, DW
Dwyer, AM
Balaraim, J
机构
[1] NASA, Langley Res Ctr, Explorat Syst Engn Branch, SED, Hampton, VA 23681 USA
[2] CALTECH, Jet Prop Lab, Pasadena, CA 91109 USA
关键词
D O I
10.2514/1.19649
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Two primary simulations have been developed and are being updated for the Mars Science Laboratory entry, descent, and landing. The high-fidelity engineering end-to-end entry, descent, and landing simulation is based on NASA Langley Research Center's Program to Optimize Simulated Trajectories II and the end-to-end real-time, hardwaee-in-the-loop simulation test bed, which is based on NASA Jet Propulsion Laboratory's Dynamics Simulator for Entry, Descent, and Surface landing. The status of these Mars Science Laboratory entry, descent, and landing end-to-end simulations at this time is presented. Various models, capabilities, as well as validation and verification for these simulations, are discussed.
引用
收藏
页码:311 / 323
页数:13
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