UH-60 Black Hawk Disturbance Rejection Study for Hover/Low Speed Handling Qualities Criteria and Turbulence Modeling

Autor:	Labows, Steven J., Blanken, Chris L., Tischler, Mark B.
Přispěvatelé:	Ames Research Center
Rok vydání:	1999
Předmět:	MOTION SIMULATION FLIGHT CONDITIONS CONTROLLABILITY HELICOPTER PERFORMANCE FLIGHT SIMULATION FLIGHT TESTS TURBULENCE LOW SPEED STABILITY HELICOPTERS HOVERING STABILITY HELICOPTER CONTROL CONTROL SIMULATION MANEUVERABILITY
Popis:	56th ; Unknown This paper will discuss the airborne flight test of the Sikorsky UH-60 Black Hawk helicopter in turbulent conditions to determine disturbance rejection criteria and develop a low speed wind/turbulence model for helicopter simulation. RTOP 581-30-22 Approved for public release; distribution is unlimited.
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=od______2778::28f76ec2d10203e7af43502e1dac587f https://hdl.handle.net/10945/60143 Zobrazit plný text záznamu