DocumentCode :
344289
Title :
Hybrid modeling for testing intelligent software for Lunar-Mars closed life support
Author :
Malin, Jane T.
Author_Institution :
Div. of Autom., Robotics & Simulation, NASA Johnson Space Center, Houston, TX, USA
Volume :
1
fYear :
1999
fDate :
36342
Firstpage :
5
Abstract :
Intelligent software is being developed for closed life support systems with biological components, for human exploration of the moon and Mars. The intelligent software functions include planning/scheduling, reactive discrete control and sequencing, management of continuous control, and fault detection, diagnosis, and management of failures and errors. The CONFIG modeling and simulation tool has been used to model components and systems involved in production and transfer of oxygen and carbon dioxide gas in a plant growth chamber and between that chamber and a habitation chamber with physico-chemical systems for gas processing. CONFIG is a multi-purpose discrete event simulation tool that integrates all four types of models, for use throughout the engineering and operations life cycle. Within CONFIG, continuous algebraic quantitative models are used within an abstract discrete event qualitative modeling framework of component modes and activity phases. Component modes and activity phases are embedded in transition digraphs. Flows and flow reconfigurations are efficiently analyzed during simulations. Modeled systems for the Life Support Testbed have included biological plants and crew members, oxygen concentrators and an oxygen transfer control subsystem, and injectors and flow controllers in a carbon dioxide control subsystem. To test the discrete control software, some elements of the lower level control layer and higher level planning layer of the intelligent software architecture are modeled, using CONFIG activity models. CONFIG simulations show effects of events on a system, including control action or failures, local and remote effects, and behavioral and functional effects, the time course of effects, and how effects may be detected. The CONFIG models are interfaced to the discrete control software layer and used to perform dynamic interactive testing of the software in nominal and off-nominal scenarios
Keywords :
aerospace control; biocontrol; chemical variables control; discrete event simulation; discrete systems; fault diagnosis; intelligent control; program testing; CONFIG modeling and simulation tool; Life Support Testbed; Lunar-Mars closed life support; abstract discrete event qualitative modeling framework; activity phases; biological components; carbon dioxide control subsystem; component modes; continuous algebraic quantitative models; continuous control; crew members; discrete control software; dynamic interactive testing; engineering life cycle; fault detection; flow controllers; flow reconfigurations; gas processing; habitation chamber; human exploration; hybrid modeling; intelligent software; moon; multi-purpose discrete event simulation tool; operations life cycle; oxygen concentrators; oxygen transfer control subsystem; physico-chemical systems; planning; plant growth chamber; reactive discrete control; scheduling; sequencing; transition digraphs; Biological control systems; Biological system modeling; Carbon dioxide; Discrete event simulation; Fault detection; Humans; Mars; Moon; Software performance; Software testing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Intelligent Processing and Manufacturing of Materials, 1999. IPMM '99. Proceedings of the Second International Conference on
Conference_Location :
Honolulu, HI
Print_ISBN :
0-7803-5489-3
Type :
conf
DOI :
10.1109/IPMM.1999.792447
Filename :
792447
Link To Document :
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