Aerospace - Vehicle Management Systems - Flight Control Design, Installation and Test of, Military Unmanned Aircraft, Specification Guide For
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.
Rationale: This document is published for the following reasons:
a. Address the need for standards and guide documents for Unmanned Aircraft onboard systems.
b. Provide recommended practices for the specification of the flight control related functions of military Unmanned Aircraft Vehicle Management Systems.
c. Recommend a method for the specification of the appropriate level of flight control capability for an Unmanned Aircraft.
d. Address the integration of the flight control functions with all other elements of the vehicle.
Included in: Unmanned Vehicles Subscription Learn More
Flight control systemsFlight control actuatorsFly-by-wire control systemsFlight management systemsSensors and actuatorsFluid power systemsHydraulic systemsElectrohydraulicsHydraulic controlHydraulic drivesHydraulic equipmentHydraulic fittingsHydraulic fluidsHydraulic motorsFuel pumpsSafetyTests and TestingAircraftMilitary aircraftUnmanned aerial vehicles
Also known as: SAE ARP 94910
Subscribers can view annotate, and download all of SAE's content.
Learn More »