This report documents the revisions made to a mathematical model of a single main rotor helicopter. These revisions were necessary to model the UH-60 helicopter accurately. The major modifications to the model include fuselage aerodynamic force and moment equations that are specific to the UH-60, a canted tail rotor, a horizontal stabilator with variable incidence, and a pitch bias actuator (PBA). In addition, the model requires a full set of parameters which describe the helicopter configuration and its physical characteristics.
Mathematical model of the UH-60 helicopter
Mathematisches Modell des UH-60-Hubschraubers
US Government Reports ; Apr ; 1-45
1984
45 Seiten
Report
English
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