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Title: Gyroscopic stable reference device

Abstract: A gyroscopic stable reference system for navigable craft is provided that provides heading, pitch, and roll outputs substantially free of errors at all aircraft attitudes.


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Inventors: Erspamer, James R. (Phoenix, AZ, US)

Application Number: 440119
Filing Date: 1974-02-06
Publication_date: 1976-01-13
Assignee: Sperry Rand Corporation (New York, NY)
Primary Class(es): 74/5.34 74/5.41
Other Classes:
US Patent Ref:
3069912Dec, 1962Faux et al.74/5.
3355954Dec, 1967Levine et al.74/5.
3456513Jul, 1969Emerson74/5.
3640137Feb, 1972Allen et al.74/5.
3648525Mar, 1972Reed74/5.

Other Refs:
Primary Examiner: Myhre, Charles J.
Assistant Examiner: Anderson, William C.
Attorney: Terry; Howard P.