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  • SAE ARP 94910 : 2012

    Current The latest, up-to-date edition.

    AEROSPACE - VEHICLE MANAGEMENT SYSTEMS - FLIGHT CONTROL DESIGN, INSTALLATION AND TEST OF, MILITARY UNMANNED AIRCRAFT, SPECIFICATION GUIDE FOR

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date:  19-12-2012

    Publisher:  SAE International

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    Table of Contents - (Show below) - (Hide below)

    1. SCOPE
    2. REFERENCES
    3. NA: USED FOR DATA OR RECOMMENDATIONS
       THAT ARE NOT AVAILABLE RECOMMENDATIONS
    4. VERIFICATION AND VALIDATION
    5. NOTES
    APPENDIX A - RECOMMENDATION APPLICABILITY
                 BY VMS TYPE

    Abstract - (Show below) - (Hide below)

    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.

    General Product Information - (Show below) - (Hide below)

    Committee A-6A3
    Document Type Standard
    Publisher SAE International
    Status Current

    Standards Referencing This Book - (Show below) - (Hide below)

    MIL-A-8865 Revision B:1987 AIRPLANE STRENGTH AND RIGIDITY MISCELLANEOUS LOADS
    MIL-PRF-7958 Revision D:2013 PUSH-PULL CONTROLS, FLEXIBLE AND RIGID
    MIL-I-8500 Revision D:1980 INTERCHANGEABILITY AND REPLACEABILITY OF COMPONENT PARTS FOR AEROSPACE VEHICLES
    SAE AS 15002 : 2010 FITTING, LUBRICATION, HYDRAULIC, SURFACE CHECK, STRAIGHT THREADS, STEEL, TYPE 2
    RTCA DO 178 : C2011 SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION
    MIL-STD-704 Revision F:2004 AIRCRAFT ELECTRIC POWER CHARACTERISTICS
    MIL-STD-130 Revision N:2007 IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY
    MIL-H-8890 Base Document:1961 HYDRAULIC COMPONENTS, TYPE 111 [65 DEGREES TO PLUS 450 DEGREES F] GENERAL SPECIFICATION FOR [ASG]
    MIL-DTL-781 Revision J:2014 TERMINAL, WIRE ROPE SWAGING, GENERAL SPECIFICATION FOR
    NASM33588:2010 NUT, SELF-LOCKING, AIRCRAFT, RELIABILITY AND MAINTAINABILITY USAGE REQUIREMENTS FOR
    SAE ARP 1281 : 2002 ACTUATORS: AIRCRAFT FLIGHT CONTROLS, POWER OPERATED, HYDRAULIC, GENERAL SPECIFICATION FOR
    MIL-STD-810 Revision G:2008 ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
    MIL-H-8891 Revision A:1978 HYDRAULIC SYSTEMS, MANNED FLIGHT VEHICLES TYPE 111 DESIGN, INSTALLATION AND DATA REQUIREMENTS FOR, GENERAL SPECIFICATION FOR
    MIL-A-87229 Base Document:1985 AUXILIARY POWER SYSTEMS, AIRBORNE
    MIL-C-18244 Revision A:1962 CONTROL AND STABILIZATION SYSTEMS, AUTOMATIC, PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL-DTL-6193 Revision E:2017 JOINTS, UNIVERSAL, PLAIN, LIGHT AND HEAVY DUTY, GENERAL SPECIFICATION FOR
    ISO 22072:2011 Aerospace — Electrohydrostatic actuator (EHA) — Characteristics to be defined in procurement specifications
    MIL-A-8870 Revision C:1993 AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE
    RTCA DO 254 : 2000 DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE
    MIL-HDBK-781 Revision A:1996 RELIABILITY TEST METHODS, PLANS, AND ENVIRONMENTS FOR ENGINEERING DEVELOPMENT, QUALIFICATION AND PRODUCTION
    MIL-M-38510 Revision J:1991 MICROCIRCUITS, SPECIFICATION FOR
    SAE AS 5440 : 2011 HYDRAULIC SYSTEMS, AIRCRAFT, DESIGN AND INSTALLATION REQUIREMENTS FOR
    MIL-HDBK-454 Revision B:2007 GENERAL GUIDELINES FOR ELECTRONIC EQUIPMENT
    SAE ARP 4493 : 2013 AEROSPACE - DIRECT DRIVE SERVOVALVES
    MIL E 5400 : T ELECTRONIC EQUIPMENT, AEROSPACE, GENERAL SPECIFICATION FOR
    MIL-STD-7080 Base Document:1994 SELECTION & INSTALLATION OF AIRCRAFT ELECTRIC EQUIPMENT
    NASM33540:2003 SAFETY WIRING, SAFETY CABLING, COTTER PINNING, GENERAL PRACTICES FOR
    SAE ARP 4761 : 1996 GUIDELINES AND METHODS FOR CONDUCTION THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT
    MIL-STD-464 Revision C:2010 ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS
    SAE AS 7997:1999 MOTORS, AIRCRAFT HYDRAULIC, CONSTANT DISPLACEMENT - GENERAL SPECIFICATION FOR
    MIL-PRF-5503 Revision G:2013 ACTUATORS: AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FOR
    MIL-HDBK-336-2 Base Document:1983 SURVIVABILITY, AIRCRAFT, NONNUCLEAR, AIRFRAME - VOLUME 2
    JSSG-2001 Revision B:2004 Air Vehicle
    MIL-STD-882 Revision E:2012 System Safety
    MIL-M-8609 Revision B:1965 MOTOR, DC 28 VOLT SYSTEM AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL-STD-461 Revision G:2015 REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT
    NASM33602:2011 BOLTS, SELF-RETAINING, AIRCRAFT, RELIABILITY AND MAINTAINABILITY, DESIGN AND USAGE REQUIREMENTS FOR
    ISO/IEC 12207:2008 Systems and software engineering Software life cycle processes
    MIL-STD-1773 Base Document:1988 FIBER OPTICS MECHANIZATION OF AN AIRCRAFT INTERNAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS
    ICAO 7300 : 9ED 2006 CONVENTION ON INTERNATIONAL CIVIL AVIATION
    MIL-A-8867 Revision C:1987 AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS
    SAE AS 94900 : 2007 AEROSPACE - FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED MILITARY AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL-A-8861 Revision B:1986 AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS
    FAA AC 120-29 : 0 CRITERIA FOR APPROVAL OF CATEGORY 1 AND CATEGORY 2 WEATHER MINIMA FOR APPROACH
    SAE AS 8775 : 1998 HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES, GENERAL SPECIFICATION FOR
    SAE AS 35411 : 2010 FITTINGS, LUBRICATION
    SAE ARP 988 : 2016 ELECTROHYDRAULIC MECHANICAL FEEDBACK SERVOACTUATORS
    MIL-S-8512 Revision D:1974 SUPPORT EQUIPMENT AERONAUTICAL, SPECIAL, GENERAL SPECIFICATION FOR THE DESIGN OF
    SAE AS 50881 : 2015 WIRING AEROSPACE VEHICLE
    MIL-M-7969 Revision C:1965 Motors, Alternating Current, 400-Cycle, 115/200-Volt System, Aircraft, General Specification for
    MIL-STD-1472 Revision G:2012 HUMAN ENGINEERING
    NASM24665:2016 PIN, COTTER (SPLIT)
    MIL-HDBK-838 Base Document:1997 LUBRICATION OF MILITARY EQUIPMENT
    SAE ARP 4386 : 2010 TERMINOLOGY AND DEFINITIONS FOR AEROSPACE FLUID POWER, ACTUATION AND CONTROL TECHNOLOGIES
    MIL-HDBK-470 Revision A:1997 DESIGNING AND DEVELOPING MAINTAINABLE PRODUCTS AND SYSTEMS - VOLUME 1
    MIL-STD-202 Revision H:2015 ELECTRONIC AND ELECTRICAL COMPONENT PARTS
    SAE ARP 4058 : 2007 GENERAL SPECIFICATION GUIDE FOR MECHANICAL GEARED ROTARY ACTUATORS
    MIL-HDBK-336-1 Base Document:1982 SURVIVABILITY, AIRCRAFT, NONNUCLEAR, GENERAL CRITERIA - VOLUME 1
    MIL-HDBK-516 Revision C:2014 AIRWORTHINESS CERTIFICATION CRITERIA
    NASM15981:2010 FASTENERS, EXTERNALLY THREADED, SELF-LOCKING DESIGN AND USAGE LIMITATIONS FOR
    MIL-HDBK-336-3 Base Document:1983 SURVIVABILITY, AIRCRAFT, NONNUCLEAR, ENGINE - VOLUME 3
    MIL-HDBK-2069 Base Document:1997 AIRCRAFT SURVIVABILITY
    SAE ARP 490 : 2008 ELECTROHYDRAULIC SERVOVALVES
    NAS 516:2015 FITTING, LUBRICATION, .1250 INCH DRIVE, FLUSH TYPE
    JSSG-2006 Base Document:1998 JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES
    RTCA DO 304 : 2007 GUIDANCE MATERIAL AND CONSIDERATIONS FOR UNMANNED AIRCRAFT SYSTEMS
    SAE AIR 1083 : 2012 AIRBORNE HYDRAULIC AND CONTROL SYSTEM SURVIVABILITY FOR MILITARY AIRCRAFT
    MIL-A-8860 Revision B:1987 AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR
    ASTM F 2501 : 2006 Standard Practices for Unmanned Aircraft System Airworthiness (Withdrawn 2015)
    MIL-STD-1553 Revision B:1978 DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA
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