Analog version of SGN-10 is self-aligning system that provides navigation and guidance data at 2 nautical mph CEP (Circular Error Probability); it also provides outputs of aircraft attitude, present latitude and longitude, and guidance to 2 destinations; system consists of inertial platform, platform electronics unit, analog computer and control and display panel; paper describes SYG-600 gyroscope and SYP-710 inertial platform on which it is mounted.
Inertial navigation system for manned aircraft
Sperry Eng Rev
Sperry Engineering Review ; 16 , n 4
1963
4 pages
Article (Journal)
English
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European Patent Office | 2021
|Emerald Group Publishing | 1964
|Engineering Index Backfile | 1964
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European Patent Office | 2021
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