| タイトル | GENIE Flight Test Results and System Overview |
| 本文（外部サイト） | http://hdl.handle.net/2060/20110004353 |
| 著者（英） | Demars, Kyle; Crain, Timothy P., II; Bishop, Robert; Paschall, Stephen, II; Brady, Tye |
| 著者所属（英） | NASA Johnson Space Center |
| 発行日 | 2011-01-01 |
| 言語 | eng |
| 内容記述 | NASA has envisioned a suite of lander test vehicles that will be flown in Earth s atmosphere to incrementally demonstrate applicable lunar lander performance in the terrestrial environment. As each terrestrial rocket progresses in maturity, relevant space flight technology matures to a higher technology readiness level, preparing it for inclusion on a future lunar lander design.. NASA s "Project M" lunar mission concept flew its first terrestrial rocket, RR1, in June 2010 in Caddo Mills, Texas. The Draper Laboratory built GENIE (Guidance Embedded Navigator Integration Environment) successfully demonstrated accurate, real time, embedded performance of Project M navigation and guidance algorithms in a highly dynamic environment. The RR1 vehicle, built by Armadillo Aerospace, performed a successful 60 second free flight and gave the team great confidence in Project M s highly reliable and robust GNC system design and implementation. This paper provides an overview of the GENIE system and describes recent flight performance test results onboard the RR1 terrestrial rocket. |
| NASA分類 | Spacecraft Design, Testing and Performance |
| レポートNO | AAS 11-084
JSC-CN-22800 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
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