Virtual Sensor Test Instrumentation, Phase II

Mobitrum has started the development of virtual sensor test instrumentation in Phase I for characterization and measurement of ground testing of propulsion systems. It is clear that future wide availability of smart sensors will significantly reduce the cost and time required to design, repair, or modify sensor systems through modular and re-configurable capability. The Phase II effort will complete the development of: 1) common sensor interface, (2) microprocessor, (3) wireless interface, (4) signal conditioning and ADC/DAC, and (5) on-board EEPROM for metadata storage and executable software to create powerful, scalable, re-configurable, and reliable distributed test instrument. The transducer senses the physical quantity being measured and converts it into an electrical signal. Then the signal is fed to an A/D converter, and is ready for use by the processor to execute functional transformation based on the sensor characteristics stored in TEDS. In order to maximize the data efficiency, a plug-and-play is required to interface with traditional sensors to enhance their identity and capabilities for data processing and communications. Virtual sensor test instrumentation is built upon open-system architecture with standardized protocol modules/stacks easily to interface with industry standards and commonly used software such as IEEE 1451, MATLAB, and LabVIEW.

This is a mature technology (TRL 7+) — the realistic path in is usually NASA's Technology Transfer Program: licensing an existing NASA patent, or a Space Act Agreement to use NASA facilities/expertise directly. NASA also runs a startup licensing program with no upfront fee for companies formed to commercialize a specific NASA technology.

None of these are guaranteed paths for this specific project — TechPort itself doesn't have an "apply" button. Reaching out to the contact(s) above with a specific question is usually the fastest way to find out what's actually open.