Criteria are given for stabilizing motion of aircraft during maneuvers involving intense rolling; qualitative results obtained in analysis are illustrated by results of calculating aircraft dynamics on digital computers and simulators; attention is given to physical explanation of results obtained and to description of mechanics of aircraft motion in common cases of controlled flight; analysis is given of reasons and conditions for appearance of phenomenon of "inertial rotation" of aircraft involving losses in effective lateral control. Translated from Mashinostroyeniye Press, Moscow, 1967. (32984)
Dynamics of spatial motion of aircraft
NASA Tech Trans
1969
210 pages
Article (Journal)
English
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