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[American Institute of Aeronautics and Astronautics Guidance and Control Conference - Seattle,WA,U.S.A. (15 August 1966 - 17 August 1966)] Guidance and Control Conference - THE ELIMINATION OF RATE GYRO ANGULAR ACCELERATION ERROR AND SCALE FACTOR SENSITIVITY TO WHEEL SPEED BY INTEGRATION OF THE OUTPUT SIGNAL

✍ Scribed by OSBAND, SIDNEY

No coin nor oath required. For personal study only.

📜 SIMILAR VOLUMES

[American Institute of Aeronautics and A

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