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タイトルCompute Element and Interface Box for the Hazard Detection System
本文(外部サイト)http://hdl.handle.net/2060/20130012668
著者(英)Khanoyan, Garen; Whitaker, William D.; Ivanov, Tonislav I.; Johnson, Andrew E.; Carson, John M.; Motaghedi, Shui H.; Vaughan, Geoffrey M.; Salomon, Phil M.; Villalpando, Carlos Y.; Some, Raphael R.; Bailey, Erik S.; Stern, Ryan A.; Martin, Keith E.; Trawny, Nikolas; Werner, Robert A.; Huertas, Andres; Goldberg, Steven B.; Spaulding, Matthew D.; Luna, Michael E.
著者所属(英)California Inst. of Tech.
発行日2013-04-01
言語eng
内容記述The Autonomous Landing and Hazard Avoidance Technology (ALHAT) program is building a sensor that enables a spacecraft to evaluate autonomously a potential landing area to generate a list of hazardous and safe landing sites. It will also provide navigation inputs relative to those safe sites. The Hazard Detection System Compute Element (HDS-CE) box combines a field-programmable gate array (FPGA) board for sensor integration and timing, with a multicore computer board for processing. The FPGA does system-level timing and data aggregation, and acts as a go-between, removing the real-time requirements from the processor and labeling events with a high resolution time. The processor manages the behavior of the system, controls the instruments connected to the HDS-CE, and services the "heavy lifting" computational requirements for analyzing the potential landing spots.
NASA分類Man/System Technology and Life Support
レポートNONPO-48786
権利Copyright, Distribution as joint owner in the copyright
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/238278


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