An analysis is presented for a family of regular extremal attitude-maneuvers for the High Angle-of-Attack Research Vehicle that has thrust-vectoring capability. Different levels of dynamic coupling are identified in the combat aircraft attitude model, and the characteristic extremal-family motion is explained. It is shown why the extremal-family trajectories develop small sideslip-angles, a highly desirable feature from a practical viewpoint.
The balance and harmony of control power for a combat aircraft in tactical maneuvering
AIAA Atmospheric Flight Mechanics Conference ; 1992 ; Hilton Head Island, SC, United States
01.01.1992
Aufsatz (Konferenz)
Keine Angabe
Englisch
Numerical simulation of maneuvering combat aircraft
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