Simplified strapped down inertial navigation utilizing bang-bang

Registers – Transfer mechanism – Traveling pawl

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244 32, 244172, G01C 2116, G06F 1550

Patent

active

040385272

ABSTRACT:
A self-contained, strapped down guidance system combining all axes, all attitude navigation having two wide angle, two-degree-of-freedom gyros which provide attitude angle and angular rate signals along three axes. Accelerometer means provide signals representative of the acceleration along three orthogonally displaced independent axes. A first transformation matrix connected to the attitude angle output of the gyros and to the accelerometers transforms the gyro and accelerometer signals from body coordinates to gyro coordinates. A second transformation matrix connected to the output of the gyros, transforms the gyro coordinates into navigation coordinates. In order to perform navigational computations, computing means compute a transformation from gyro momentum vector (referenced to coordinate frame) to a navigational coordinate frame such as a locally vertical frame wherein the Z axis is always along the local vertical direction.

REFERENCES:
patent: 3231726 (1966-01-01), Williamson
patent: 3272972 (1966-09-01), Yamron
patent: 3374966 (1968-03-01), Howard
patent: 3597598 (1971-08-01), McAllister et al.
patent: 3924824 (1975-12-01), Brodie et al.

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