Resonatorkreisel mit Dualem Vibrationsmuster

EP3330665 Art B1 6. Juli 2022

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
Offizieller Volltext

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
🇺🇸 Northrop Grumman

US-amerikanischer Rüstungs- und Luftfahrtkonzern mit Sitz in Virginia, tätig in den Bereichen Verteidigungselektronik, Flugzeugbau, Raumfahrt und Cybersicherheit.

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