THE DYNAMICS OF FLIGHT STABILITY AND CONTROLLABILITY OF FLYING VEHICLES,

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Abstract:

The book is devoted to the theory of stability and controllability of flying vehicles. The stability and controllability of winged flying vehicles is the basic subject for a wide range of velocities, including supersonic velocities. The book discusses contemporary methods of investigating stability and controllability in longitudinal and lateral motions, on takeoff and landing and in critical angles of attack. The transfer functions for a flying vehicle are considered, as are the methods for selecting optimum vehicle and automation parameters. In addition to the mathematical foundations of the studies, engineering methods for the computation of stability and controllability with numerical examples are presented. Author

Author(s):
Ostoslavskii, I. V. ; Strazheva, I. V.
Author Organization(s):
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Supplementary Note:
Unedited rough draft trans. of mono. Dinamika Poleta Ustoichivost i Upravlyaemost Letatelnykh Apparatov, Moscow, 1965 467p.
Annotation:
Translation of Russian research: The dynamics of flight stability and controllability of flying vehicles.
Pagination:
0700

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
FTD-HT-66-282, TT-67-61394
Monitor Series:
67-61394
 Subject Terms
Communities of Interest:
No COI(s) Identified
Descriptor(s):
(*AIRCRAFT, FLIGHT), (*FLIGHT, AERODYNAMIC CHARACTERISTICS), STABILITY, CONTROL, AEROELASTICITY, ANGLE OF ATTACK, FORCE(MECHANICS), EQUATIONS OF MOTION, MATHEMATICAL ANALYSIS, USSR
Field(s)/Group(s):
Aerodynamics
Report Date:
1966 Dec 12