Inertial navigation system including self-contained performance

Details Inertial navigation system including self-contained performance Inertial navigation system including self-contained performance

1992-06-11

1994-04-05

Black, Thomas G.

Boots, shoes, and leggings

342358, 73 1E, 73178R, 364559, H04B 7185, G06F 1550

Patent

active

053011147

ABSTRACT:
The accuracy of the performance of an inertial navigation system is validated by comparing data measured by a fourth gyro and accelerometer to an analytic equivalent constructed from measurements made by a primary gyro/accelerometer orthogonal triad.

REFERENCES:
patent: 4280188 (1981-07-01), Weinstein et al.
patent: 5067084 (1991-11-01), Kau
patent: 5194872 (1993-03-01), Mosuff et al.
Harrison, J. V. and E. G. Gai, `Evaluating Sensor Orientations for Navigation Performance and Failure Detection`, Nov. 1977, pp. 631-643.
Gelb, A., `Synthesis of a Very Accurate Inertial Navigation System`, Jun. 1965, pp. 119-128.
Morrell, F. R. & Motyka, P., `Unified Analysis Methods for a Fault Tolerant Redundant Strapdown Inertial Navigation Unit`, Oct. 1983, 21.6.1-21.6.10.

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