Method for compensating a Coriolis gyroscope quadrature bias and a coriolis gyroscope for carrying out said method
Details for Australian Patent Application No. 2004312572 (hide)
International Classifications
Event Publications
17 August 2006 PCT application entered the National Phase
PCT publication WO2005/066585 Priority application(s): WO2005/066585
7 February 2008 Application Accepted
Published as AU-B-2004312572
5 June 2008 Standard Patent Sealed
8 January 2009 Alteration of Name
The name of the patentee has been altered to Northrop Grumman LITEF GmbH 2005
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