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Spacecraft Lighting Network System TOPIC# - TDC-46-F17

Background:

Currently, spacecraft lighting system are operated independently through switches and knobs. For future deep space missions, spacecrafts will require new and innovative intelligent light control methods to minimize power, improve reliability such as compensating for degrading lighting sources, and provide lighting necessary for the biological aspect of the human. Therefore, it is highly desired that spacecraftlighting system have the ability to communicate on a networkwith on-board computers for determining lighting health status aswell as controlling the lighting spectrum for task activities and maintaining circadian rhythmsof the crew.

Project Description:

Currently, commercial lighting bus standard chipsets are not suitable for the deep space radiation environment. The focus of this project is to implement the DMX512 lighting standard using programmable computer devices such as microcontrollers or field programmable gate arrays. The reason for implementing in programmable devices is that radiation tolerant/hardened (Rad Tol/Hrd) programmable devices exist such that the standard could be implemented in a Rad Tol/Hrd device(s). This proof of concept would show the feasibility of implementing in a programmable device. The proof of concept DMX512 network bus should:

  • Use commercial programmable devices as this is a proof-of-concept
  • Ability to communicate with the SLNS over Ethernet
  • Source of power is AC
  • Control at least two RGB lighting sources and accept one light sensor data over the bus.
  • GUI to control the SLNS
  • Program menu for selecting should include at least
    • (1) health status of the lighting source such as lighting intensity compare what is programmed to what sensors detect and different lighting
    • (2) control lighting intensity
    • (3) Provisions for expanding the number of DMX deviceson the bus.
  • Enclosure to house the SLNS with standard I/O connectors