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- W2081170677 abstract "A general theoretical model is used in order to investigate the possibility of an active aerodynamic stabilization of a helicopter/sling-load system in the case of a single suspension point. The stabilization system includes two vertical aerodynamic surfaces that are located on the external sling load. The incidence angles of these surfaces are varied according to a set of control laws. This study leads to a system that is relatively easy to realize. The input measurements of the load stabilization system (LSS) include the helicopter and sling load lateral/directional angular rates. It is shown that adding a feedback loop that is based on the load lateral acceleration increases further the stability of the whole system. Studies also show that a single rear surface is very efficient and can be used alone. The proposed LSS is capable of stabilizing the system in a wide range of airspeeds, load weights, suspension methods (geometries), and aerodynamic properties of the external sling load." @default.
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- W2081170677 date "1989-09-01" @default.
- W2081170677 modified "2023-10-14" @default.
- W2081170677 title "Active aerodynamic stabilization of a helicopter/sling-load system" @default.
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- W2081170677 doi "https://doi.org/10.2514/3.45847" @default.
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