||About the Author|Jayanth Krishnamurthi obtained a dual B.S. in Mechanical and Aerospace Engineering from the Rensselaer Polytechnic Institute (RPI) in December 2009. Subsequently, he obtained an M.S. in Aerospace Engineering from The Pennsylvania State Universi
A control design method to address low-speed stability and handling qualities issues of helicopter slung load operations is presented. A simple model was developed using first principle physics with application of basic control techniques to understand the couple dynamics. Subsequently, a non-linear slung load model was developed and integrated with the GenHel-PSU simulation of the UH-60A. Linear model frequency responses were verified against AFDD OVERCAST models and f...
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