Computer program compares various control-system concepts for improving handling qualities of single-rotor helicopters carrying relatively-large external sling loads. Computer program developed to test these and other ideas helps to circumvent expensive prototype and field testing. Comparisons between (1) computed data and flight data, (2) simulation-system values and flight test data, and (3) pilot evaluations of simulation and actual-flight conditions are very favorable.
Helicopter sling loads
NASA Tech Briefs ; 4 , 4
1980-06-01
Sonstige
Keine Angabe
Englisch
A method of automatically stabilizing helicopter sling loads
TIBKAT | 1974
|Flight Director for Handling of Helicopter Sling Loads
British Library Conference Proceedings | 2005
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