DARPA Develops New Fabrication Methods for Microscale Inertial Sensors

DARPA is devising new and low-cost fabrication techniques for microscale inertial sensors to improve their precision and help replace the existing gyroscopes. Under the MRIG (Microscale Rate Integrating Gyroscope) effort of the Micro-PNT (Micro-Technology for Positioning, Navigation and Timing) program, this initiative is being carried out.

The first phase was accomplished recently, where MRIG targeted nontraditional materials-based 3-D microfabrication techniques. Fabrication of small 3-D structures like hemispheres, wineglass-shaped structures and toroids were achieved, transforming from the 2-D paradigm of contemporary microgyroscopes.

The operation of microscale inertial sensors resembles Foucault pendulums in museums. Rather than a swinging pendulum, microscale inertial sensors transmit vibrations through the surface of a 3-D structure. Evaluation on the precession of the standing wave is done and any alteration will impact the orientation. For integrated operation with the microscale inertial sensors, DARPA has developed new fabrication methods such as:

• Glass-blowing: Inspired by the traditional glass-blowing techniques at the microscale, very small 3-D wineglass-shaped inertial sensors were created. These sensors are symmetrical and have frequency split up to 10 hz.
• Blown quartz: Resembling glass blowing, quartz blowing is effective for creating more symmetric structure. Scientists designed fabrication techniques that can heat quartz to 1,7000 C followed by rapid cooling. The fabrication is performed in massive batches, resulting in several devices on a single wafer.
• Atomic layering of diamond: Depositing CVD diamond in a micro-well on the substrate or layering diamond over a blown structure was successful, leading to highly symmetric, precise 3-D inertial-sensor structures.

Phase 2 performers focus on developing these devices, where their precision and reliability were enhanced by decreasing frequency split from 10 Hz to 5 Hz, decreasing volume from 20 to 10 mm³, and by raising decay times from 10 to 100 sec. Demonstration of a unique, working microrate integrating gyroscope is the final objective of Phase 2.

Source: http://www.darpa.mil/

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