Hodographs are obtained from analysis of roots of inertial system computer equations for errors in determining coordinates of longitudinal and lateral motion of flight vehicle, which correspond to angular velocity variation over total possible range; qualitative study of inertial-system properties for high speed flight; results obtained for velocity of 8 km/sec are compared with known theory in celestial mechanics. (see also English translation in Eng Cybernetics n 2 Mar-Apr 1965 p 158-69)
Analysis of inertial systems of navigation for high speed flight
Povedenie inertsial'nykh sistem navigatsii pri bol'shikh skorostyakh poleta
1965
12 pages
Article (Journal)
Russian
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Analysis of inertial systems of navigation for high speed flight
Engineering Index Backfile | 1965
|Inertial navigation systems analysis.
NTRS | 1971
|