Resonatorkreisel mit Dualem Vibrationsmuster
Anmelder: Northrop Grumman Systems Corporation 🇺🇸
Details
- Veröffentlichungs-Nr.
- EP3330665
- Aktenzeichen
- EP17202551
- Anmeldetag
- 20. November 2017
- Veröffentlichung
- 6. Juli 2022
- Erteilung
- 6. Juli 2022
- Rechtsraum
- EP
- IPC
- G01C19/5677// G01C25/00
Abstract
One example includes a resonator gyroscope (10). The resonator gyroscope includes a sensing system (12, 50) comprising a plurality of electrodes (18, 54, 56, 58, 60, 62, 64, 66, 68) arranged about a sensitive axis (70) and configured to electrostatically force a resonator (16) into a substantially periodic motion based on a plurality of forcer signals (FRC) applied to the plurality of electrodes (18, 54, 56, 58, 60, 62, 64, 66, 68), and configured to provide an indication of rotation (ROT) about a sensitive axis (70) of the resonator gyroscope (10). The resonator gyroscope (10) further includes a controller (14) configured to generate the plurality of forcer signals (FRC) to provide the substantially periodic motion of the resonator (16) concurrently in each of a plurality of separate vibration pattern modes to measure the rotation (ROT) of the resonator gyroscope (10) about the sensitive axis (70) in response to a plurality of pickoff signals (PO) associated with the substantially periodic motion.
Anmelder
- Firma
- Northrop Grumman Systems Corporation
- Land
- 🇺🇸 USA
US-amerikanischer Rüstungs- und Luftfahrtkonzern mit Sitz in Virginia, tätig in den Bereichen Verteidigungselektronik, Flugzeugbau, Raumfahrt und Cybersicherheit.
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