Measuring and testing – Speed – velocity – or acceleration – Response to multiple sensing means or motion conditions
Reexamination Certificate
2005-09-27
2005-09-27
Chapman, John E. (Department: 2856)
Measuring and testing
Speed, velocity, or acceleration
Response to multiple sensing means or motion conditions
C318S649000, C244S003200
Reexamination Certificate
active
06948367
ABSTRACT:
An accelerometer includes an inertial platform maintaining an attitude in response to a platform stabilizing controller signal and defining a spin axis and a reference plane. An accelerometer, coupled to the inertial platform a distance from the spin axis, defines a flex axis. The accelerometer generates an accelerometer signal in response to acceleration of the accelerometer. A second accelerometer defines a second flex axis, and is also coupled to the inertial platform a distance from the spin axis. The second accelerometer generates a second accelerometer signal in response to acceleration of the second accelerometer. A controller receives the first accelerometer signal and the second accelerometer signal and generates a linear acceleration signal in response to a sum of the first accelerometer signal and the second accelerometer signal and generates an angular acceleration signal from the difference. The controller further generates the platform stabilizing controller signal in response to the first acceleration signal and the second acceleration signal.
REFERENCES:
patent: 4601206 (1986-07-01), Watson
patent: 5124938 (1992-06-01), Algrain
patent: 5383363 (1995-01-01), Kulmaczewski
patent: 6776043 (2004-08-01), Campbell et al.
Campbell Ray F.
Wada Joan D.
Artz & Artz PC
Chapman John E.
The Boeing Company
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