A real-time compensation system of a projectile includes at least one flight controller, at least one imager device, at least one gyroscope, and at least one processor. The at least one flight controller is configured to rotate the projectile about an axis between a first orientation and a second orientation. The at least one imager device is configured to capture a first image at the first orientation and a second image at the second orientation. The at least one gyroscope is configured to sense a first angular rate of the projectile as the projectile rotates from the first orientation to the second orientation. The at least one processor is configured to determine a first rotation angle based upon the first and second images and a second rotation angle based upon the angular rate sensed by the at least one gyroscope, and determine a gyroscope compensation parameter.
REAL-TIME COMPENSATION OF INERTIAL GYROSCOPES
ECHTZEITKOMPENSIERUNG VON TRÄGHEITSGYROSKOPEN
COMPENSATION EN TEMPS RÉEL DE GYROSCOPES INERTIELS
2021-04-28
Patent
Electronic Resource
English
On the Inertial Measurement Unit Using Fiber Optic Gyroscopes
British Library Conference Proceedings | 1996
|British Library Conference Proceedings | 1994
|AIAA | 2001
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