U.S. patents available from 1976 to present.
U.S. patent applications available from 2005 to present.

Accelerometer system

Patent 4601206 Issued on July 22, 1986. Estimated Expiration Date: Icon_subject September 14, 2004. Estimated Expiration Date is calculated based on simple USPTO term provisions. It does not account for terminal disclaimers, term adjustments, failure to pay maintenance fees, or other factors which might affect the term of a patent.

Patent References

2996268

Inventor

Assignee

Application

No. 06/650648 filed on 09/14/1984

US Classes:

73/510, Response to multiple sensing means or motion conditions73/514.02Angular acceleration

Examiners

Primary: Ciarlante, Anthony V.

Attorney, Agent or Firm

International Classes

G01C 21/10 (20060101)
G01P 15/18 (20060101)
G01P 15/08 (20060101)
G01C 21/16 (20060101)

Foreign Application Priority Data

1983-09-16 GB

Abstract

An inertial platform accelerometer cluster (FIG. 1) comprises a cluster of gyro and accelerometer system triads disposed in a cluster housing 10 to detect motion along and about orthogonal x, y and z axes. The orthogonal accelerometer systems each comprises a pair of codirectional accelerometers e.g. 15x, 15'x having an operating bandwidth from 0 to several KHz mounted on the housing walls equidistant from a point 14, which represents a common center of percussion to all pairs, at the center of gravity of the cluster. The analogue output signals of each accelerometer pair are scaled, summed and differenced to provide `sum` and `difference` signals which represent respectively acceleration in the sensitive direction and angular acceleration about an orthogonal axis. The sum and difference signals can be used in analogue correction generating circuitry to obtain correction signals for coning and sculling effects, for which responses at high-frequency are called for, while economizing on computer time and capacity. Furthermore the coincidence of the center of percussion for all accelerometer pairs eliminates size effect errors from the `sum` signal which is employed for the normal inertial platform computations. Separate high- and low-frequency responsive accelerometers may be used.

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