A method of fabricating a gyroscope may involve depositing conductive material on a substrate, forming an anchor on the substrate, forming a drive frame on the anchor and forming pairs of drive beams on opposing sides of the anchor. The drive beams may be configured to constrain the drive frame to r
A method of fabricating a gyroscope may involve depositing conductive material on a substrate, forming an anchor on the substrate, forming a drive frame on the anchor and forming pairs of drive beams on opposing sides of the anchor. The drive beams may be configured to constrain the drive frame to rotate substantially in the plane of the drive beams. The method may involve forming a proof mass around the drive frame and forming a plurality of sense beams that connect the drive frame to the proof mass. The sense beams may be tapered sense beams having a width that decreases with increasing distance from the anchor. The tapered sense beams may be configured to allow sense motions of the proof mass in a sense plane substantially perpendicular to the plane of the drive beams in response to an applied angular rotation. Some components may be formed from plated metal.
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1. A method of fabricating a gyroscope, the method comprising: depositing conductive material on a substrate;forming an anchor on the substrate;forming a drive frame on the anchor;forming pairs of drive beams on opposing sides of the anchor, the drive beams connecting the drive frame to the anchor,
1. A method of fabricating a gyroscope, the method comprising: depositing conductive material on a substrate;forming an anchor on the substrate;forming a drive frame on the anchor;forming pairs of drive beams on opposing sides of the anchor, the drive beams connecting the drive frame to the anchor, the drive beams being configured to constrain the drive frame to rotate substantially in a plane of the drive beams;forming a proof mass around the drive frame; andforming a plurality of sense beams that connect the drive frame to the proof mass, the sense beams being tapered sense beams having a width that decreases with increasing distance from the anchor, the tapered sense beams being configured to allow sense motions of the proof mass in a sense plane substantially perpendicular to the plane of the drive beams in response to an applied angular rotation. 2. The method of claim 1, wherein forming the drive beams includes the following: depositing a first metal layer that is in contact with the conductive material;depositing a piezoelectric layer on the first metal layer;depositing a second metal layer on the piezoelectric layer; andforming a third metal layer on the second metal layer. 3. The method of claim 2, wherein forming the third metal layer involves electroplating. 4. The method of claim 3, wherein the electroplating involves depositing metal for the proof mass and the tapered sense beams. 5. The method of claim 3, further including separating the substrate into a plurality of sub-panels prior to the electroplating. 6. The method of claim 2, wherein forming the third metal layer involves forming the third metal layer to a thickness of tens of microns. 7. The method of claim 2, wherein forming the third metal layer involves forming at least one of nickel, nickel-iron, nickel-cobalt, nickel-manganese, cobalt-iron, nickel-tungsten, palladium-nickel or palladium-cobalt on the second metal layer. 8. The method of claim 2, further comprising: depositing a gold layer on the third metal layer. 9. The method of claim 1, wherein forming the anchor includes: etching through a sacrificial layer to expose a first metal layer;depositing an oxide layer on the first metal layer;forming a seed layer on the oxide layer; andelectroplating a second metal layer on the seed layer. 10. The method of claim 9, wherein forming the seed layer involves forming at least one of nickel, a nickel alloy, copper or an alloy of chrome and gold on the oxide layer. 11. The method of claim 1, further comprising: encapsulating the gyroscope inside packaging. 12. The method of claim 11, wherein the encapsulating involves sealing the gyroscope inside the packaging. 13. The method of claim 12, wherein the sealing involves sealing the gyroscope substantially in a vacuum. 14. The method of claim 11, further comprising: forming a portion of the conductive material into an electrical connection from the gyroscope inside the packaging to an area outside of the packaging. 15. The method of claim 11, further comprising: forming a seal ring, wherein the encapsulating involves attaching a cover to the seal ring. 16. The method of claim 15, wherein the cover includes metal or glass. 17. The method of claim 15, further comprising: forming an electrical pad outside of the seal ring, the electrical pad being capable of electrical connection with the conductive material. 18. The method of claim 1, wherein forming the proof mass and forming the drive frame involves: etching between a drive frame area and a proof mass area;depositing high aspect ratio photoresist material between the drive frame area and the proof mass area; andelectroplating a metal layer in the drive frame area and the proof mass area. 19. The method of claim 18, wherein forming the proof mass and forming the drive frame also involves: removing the high aspect ratio photoresist material from between the drive frame area and the proof mass area;etching to expose a sacrificial layer disposed below the drive frame and the proof mass; andremoving the sacrificial layer to release the drive frame and the proof mass.
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