Standard

IEEE 292

Published

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Abstract

This specification defines the requirements for a single-degree-of-freedom spring-restrained rate gyro for [aircraft, missile, spacecraft,______] applications. The rate gyro shall be capable of providing [(dc, ac) voltage outputs proportional to angular rate inputs up to______ degrees per second, a switch closure(s) at angular rates (exceeding, less than)______ (+, - , ± )______ degrees per second].

Document information

  • Standard from IEEE_AC
  • Published:
  • Version: 0
  • Document type: IS