Handling qualities evaluation of an automatic slung load stabilization system for rescue hoist operations

The Handling Qualities (HQs) of a helicopter can be adversely affected through the presence of an externally slung load. Helicopter stability margins may be reduced, due to the additional dynamics of the load system, which can subsequently increase pilot workload, and reduce the operational envelope...

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Veröffentlicht in:	CEAS aeronautical journal 2016-12, Vol.7 (4), p.587-606
Hauptverfasser:	Nonnenmacher, D., Jones, M.
Format:	Artikel
Sprache:	eng
Schlagworte:	Active control Aerospace Technology and Astronautics Automatic pilots Damping Dynamic stability Engineering Flight simulation Flight tests Loads (forces) Original Paper Oscillations Simulation Stabilization
Online-Zugang:	Volltext
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