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Computational Modeling to Limit the Impact Displays and Indicator Lights Have on Habitable Volume Operational Lighting ConstraintsThe goal of this investigation is to determine design limitations and architectural solutions that limit the impact light from displays and indicator lamps have on the operational environment task lighting and lighting countermeasure spectrum constraints. It is concerning that this innovative architectural lighting system, could be compromised by spectrums from display systems, architectural materials, and structures that are not considered as part a full system design implementation. The introduction of many Commercial Off the Shelf (COTS) products to the spacecraft volume that contain LEDs, without consideration to the human factors and biological constraints, is another problem. Displays and indicators are a necessary part of the spacecraft and it is the goal of this research project to determine constraints and solutions that allow these systems to be integrated while minimizing how the lighting environment is modified by them. Due to the potentially broad scope of this endeavor, the project team developed constraints for the evaluation. The evaluation will be on a set of tasks that required significant exposure in the same environment while having a large chance of impacting the light spectrum the crew is expected to receive from the architectural lighting system. The team plans to use recent HRP research on "Net Habitable Volume" [1] to provide the boundary conditions for volume size. A Zemax ® lighting model was developed of a small enclosure that had high intensity overhead lighting and a standard intensity display with LED indicator arrays. The computer model demonstrated a work surface illuminated at a high level by the overhead light source compared to displays and indicators whose light is parallel to the work plane. The overhead lighting oversaturated spectral contributions from the display and indicator at the task work surface. Interestingly, when the observer looked at the displays and LEDs within the small enclosure, their spectral contribution was significant but could be reduced by reflecting overhead light from the wall(s) to the observer. Direct observation of displays and LEDs are an issue because the user's viewing area is a display, not an illuminated work surface. Since avionics command centers consume significant crew time, the tasks that seemed at higher risk for unwanted spectral contributions as an operational volume with significant quantity of displays and indicators that were either under direct observation of the crew or impacting a volume the crew may be required to sleep in.
Document ID
20150020938
Acquisition Source
Johnson Space Center
Document Type
Abstract
Authors
Clark, T. E.
(Lockheed Martin Corp. Houston, TX, United States)
Salazr, G. A
(NASA Johnson Space Center Houston, TX, United States)
Brainard, G. C.
(Thomas Jefferson Univ. Philadelphia, PA, United States)
Date Acquired
November 6, 2015
Publication Date
February 8, 2016
Subject Category
Spacecraft Design, Testing And Performance
Man/System Technology And Life Support
Report/Patent Number
JSC-CN-34594
Meeting Information
Meeting: 2016 HRP Investigators Workshop
Location: Galveston, TX
Country: United States
Start Date: February 8, 2016
End Date: February 11, 2016
Distribution Limits
Public
Copyright
Public Use Permitted.
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