Modeing of a helicopter with an under-slung load system

Abstract

This paper considers modeling and simulation study of a helicopter with an under-slung external load system. Mathematical models of a single main rotor helicopter and an under-slung load are presented in this paper. Considering the two models, a mathematical model for a helicopter carrying an under-slung load is obtained. The combined system model can be used for stability analysis and controller development to improve system performance.

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