• ARP94910

• 2012-12-19

• A-6a3 Flight Control Systems Committee

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.

• SAE ARP 94910

• Aerospace

• Flight control systems
• Flight control actuators
• Fly-by-wire control systems
• Flight management systems
• Sensors and Actuators
• Fluid power systems
• Hydraulic systems
• Electrohydraulics
• Hydraulic control
• Hydraulic drives
• Hydraulic equipment
• Hydraulic fittings
• Hydraulic fluids
• Hydraulic motors
• Fuel pumps
• Safety
• Tests and Testing
• Aircraft
• Military aircraft
• Unmanned aerial vehicles