Accession Number : AD0516838
Title : Design of an Experimental Development Multiple Rotation Gyroscope.
Descriptive Note : Technical rept. 15 May 68-15 Feb 71,
Corporate Author : SPERRY RAND CORP GREAT NECK NY SPERRY GYROSCOPE
Personal Author(s) : Quermann, T. R. ; Ziegler, H. M.
Report Date : JUN 1971
Pagination or Media Count : 96
Abstract : The significance of this research and development program to the Air Force is that a gyro is being developed that does not depend on its accuracy being achieved through ultra-precision fabrication of parts and extensive test and calibration. Hence, the result will be a gyro with stable and repeatable performance under adverse environments, in addition to lower cost and higher reliability. The prime objectives of this follow-on program were the continued development of the Multiple Rotation Gyroscope (MRG) concept and the experimental demonstration of the performance capability of a given configuration. Evaluations of several iterations of an engineering model MRG at both gyro and platform levels led to the identification and reduction of certain error mechanisms, and in the final configuration yielded excellent test data. Based on these encouraging test results, preliminary design information was prepared for an extremely simple embodiment of the MRG principle. (Author)
Descriptors : (*GYROSCOPES, DESIGN), MULTIPLE OPERATION, ROTATION, GAS BEARINGS, PNEUMATIC DEVICES, HYDRAULIC EQUIPMENT, LIQUIDS, HYDRODYNAMICS, FLOATING BODIES, AIR FORCE RESEARCH, DRIFT, KINEMATICS, COSTS.
Subject Categories : Navigation and Guidance
Distribution Statement : APPROVED FOR PUBLIC RELEASE