A fixed base manned V/STOL handling qualities simulation was performed to investigate 1) classification criteria of attitude and rate command systems in hover and low-speed flight; 2) control system blending schemes for transition from approach dynamics to hover dynamics and vice versa, and 3) the amount of control usage. Pilot ratings and comments showed that a time response criterion discriminated well between attitude and rate systems; blending schemes for transition correlated well with earlier NASA results and; pilot's command gain had a strong effect on piloting characteristics and the amount of control usage. (Author)
V/STOL (Vertical/Short Takeoff and Landing) Low Speed and Transition Equivalent Systems Analysis
1982
193 pages
Report
Keine Angabe
Englisch
Aircraft , Aeronautics , Vertical takeoff aircraft , Short takeoff aircraft , Flight maneuvers , Low velocity , Hovering , Attitude(Inclination) , Rates , Flight control systems , Blending , Transitions , Aircraft landings , Flight simulation , Carrier based aircraft , Systems analysis , Naval aircraft , Flying qualities , Low speed flight
The physics of short takeoff and landing /STOL/
AIAA | 1970
|Europäisches Patentamt | 2023
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