SAE ARP94910-2012 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.
SAE ARP94910-2012 Referenced Document
ASTM F2395-07 Standard Terminology for Unmanned Air Vehicle Systems *, 2024-04-20 Update
ASTM F2501-06 Standard Practices for Unmanned Aircraft System Airworthiness *, 2024-04-20 Update
IEEE 1394.3-2003 A High Performance Serial Bus Peer-to-Peer Data Transport Protocol (PPDT) (IEEE Computer Society Document)
ISO 22072:2011 Aerospace - Electrohydrostatic actuator (EHA) - Characteristics to be defined in procurement specifications
ISO/IEC 12207:2008 Systems and software engineering - Software life cycle processes
SAE AS5440-1998 Hydraulic Systems, Aircraft, Design and Installation Requirements for FSC 1650; Should Be Used Instead of MIL-H-5440H, Which Was Cancelled on 13 September 1999
SAE AS7997-1999 Motors, Aircraft Hydraulic, Constant Displacement General Specification for FSC 1650
SAE ARP94910-2012 history
2012SAE ARP94910-2012 Aerospace - Vehicle Management Systems - Flight Control Design, Installation and Test of, Military Unmanned Aircraft, Specification Guide for