Inertial navigation system including self-contained performance validating arrangement
First Claim
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1. An inertial navigation system including a self-contained performance validating arrangement, comprising:
- an inertial sensor assembly including a substantially orthogonal triad having three gyros and three accelerometers;
said inertial sensor assembly including a fourth gyro and a fourth accelerometer having input axes which symmetrically bisect the input axes of the orthogonal triad;
means for establishing an analytical equivalent to data from the fourth gyro and the fourth accelerometer from measurements made by the orthogonal triad including means for providing compensated incremental angle vectors, means for providing compensated incremental velocity vectors, and means for transforming the incremental angle vectors and the incremental velocity vectors to an analytical equivalent measurement along the axes of the fourth gyro and the fourth accelerometer, respectively; and
means for comparing data from the fourth gyro and the fourth accelerometer to said analytical equivalent for validating the performance of the inertial navigation system.
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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.
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Citations
10 Claims
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1. An inertial navigation system including a self-contained performance validating arrangement, comprising:
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an inertial sensor assembly including a substantially orthogonal triad having three gyros and three accelerometers; said inertial sensor assembly including a fourth gyro and a fourth accelerometer having input axes which symmetrically bisect the input axes of the orthogonal triad; means for establishing an analytical equivalent to data from the fourth gyro and the fourth accelerometer from measurements made by the orthogonal triad including means for providing compensated incremental angle vectors, means for providing compensated incremental velocity vectors, and means for transforming the incremental angle vectors and the incremental velocity vectors to an analytical equivalent measurement along the axes of the fourth gyro and the fourth accelerometer, respectively; and means for comparing data from the fourth gyro and the fourth accelerometer to said analytical equivalent for validating the performance of the inertial navigation system. - View Dependent Claims (2)
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3. An inertial navigation system including a self-contained performance validating arrangement, comprising:
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an inertial sensor assembly including a substantially orthogonal triad having three gyros and three accelerometers; said inertial sensor assembly including a fourth gyro and a fourth accelerometer having input axes which symmetrically bisect the input axes of the orthogonal triad; means for establishing an analytical equivalent to data from the fourth gyro and the fourth accelerometer from measurements made by the orthogonal triad; means for comparing data from the fourth gyro and the fourth accelerometer to said analytical equivalent for validating the performance of the inertial navigation system; means for summing the transformed incremental angle vectors and for providing a first summation output; means for summing the transformed incremental velocity vectors and for providing a second summation output; means for summing the incremental bisector angles from the fourth bisector gyro and for providing a third summation output; means for summing the incremental bisector velocities from the fourth bisector accelerometer and for providing a fourth summation output; means for taking the differences between the first and third summation outputs, said differences corresponding to an angle error criteria; and means for taking the differences between the second and fourth summation outputs, said differences corresponding to a velocity error criteria. - View Dependent Claims (4, 5)
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6. A self-contained method for validating the performance of an inertial navigation system, comprising:
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providing an inertial sensor assembly with a substantially orthogonal triad having three gyros and three accelerometers; providing a fourth gyro and a fourth accelerometer having input axes which symmetrically bisect the input axes of the orthogonal triad; establishing an analytical equivalent to data from the fourth gyro and the fourth accelerometer from measurements made by the orthogonal triad including establishing compensating incremental angle vectors, establishing compensated incremental velocity vectors, and transforming the incremental angle vectors and the incremental velocity vectors to an analytical equivalent measurement along the axes of the fourth gyro and the fourth accelerometer, respectively; and comparing data from the fourth gyro and the fourth accelerometer to said analytical equivalent for validating the performance of the inertial navigation system. - View Dependent Claims (7, 8, 9, 10)
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Specification