The effect of geometric and aerodynamic characteristics on the stability of the lateral degrees of freedom of a typical helicopter sling load is examined. The feasibility of stabilizing the suspended load by controllable fins was also studied. Linear control theory was applied to the design of a simple control law that stabilized the load over a wide range of helicopter airspeeds.
A method of automatically stabilizing helicopter sling loads
1974-07-01
Sonstige
Keine Angabe
Englisch
A method of automatically stabilizing helicopter sling loads
TIBKAT | 1974
|NTRS | 1980
|Flight Director for Handling of Helicopter Sling Loads
British Library Conference Proceedings | 2005
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