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SAE ARP94910
Aerospace - Vehicle Management Systems - Flight Control Design, Installation and Test of, Military Unmanned Aircraft, Specification Guide For
Печатная копияПечатное изданиеЭлектронный (pdf)
149.40 $ (включая НДС 20%)
Зарубежные/Группа SAE/SAE
Flight control systemsHydraulic drivesHydraulic equipmentHydraulic fittingsHydraulic fluidsHydraulic motorsFuel pumpsSafetyTests and TestingAircraftMilitary aircraftFlight control actuatorsUnmanned aerial vehiclesFly-by-wire control systemsFlight management systemsSensors and actuatorsFluid power systemsHydraulic systemsElectrohydraulicsHydraulic control
This document establishes recommended practices for the specification of general performance, design, test, development, and quality assurance requirements for the flight control related functions of the Vehicle Management Systems (VMS) of military Unmanned Aircraft (UA), the airborne element of Unmanned Aircraft Systems (UAS), as defined by ASTM F 2395-07. The document is written for military unmanned aircraft intended for use primarily in military operational areas. The document also provides a foundation for considerations applicable to safe flight in all classes of airspace.