Redundant inertial measurement system configuration

Details Redundant inertial measurement system configuration Redundant inertial measurement system configuration

1974-06-17

1977-05-03

Myhre, Charles J.

Machine element or mechanism

Gyroscopes

Multiple gyroscopes

G01C 1902

Patent

active

040207021

ABSTRACT:
A redundant inertial measuring system includes three strapdown platforms each having two inertial sensors. The sensitive axes of the sensors are discretely disposed relative to the faces of a dodecahedron. The sensors and their associated electronics are physically and electrically separated from each other within each of the platforms.

REFERENCES:
patent: 3282119 (1966-11-01), Shaw, Jr. et al.
patent: 3477298 (1969-11-01), Howe
patent: 3489004 (1970-01-01), Barnhill et al.
patent: 3563662 (1971-02-01), Wing
Journal of Spacecraft and Rockets vol. 9, No. 1, Jan. 1972 article entitled "A Redundant Strapdown Inertial Reference Unit (SIRU)" pp. 39-47.

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