SAE ARP94910
Current
The latest, up-to-date edition.
Aerospace - Vehicle Management Systems - Flight Control Design, Installation and Test of, Military Unmanned Aircraft, Specification Guide For
Hardcopy , PDF
English
19-12-2012
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
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.
| DocumentType |
Standard
|
| Pages |
113
|
| PublisherName |
SAE International
|
| Status |
Current
|
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.
| 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 AS15002C | FITTING, LUBRICATION, HYDRAULIC, SURFACE CHECK, STRAIGHT THREADS, STEEL, TYPE II |
| 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 III (-65 Degrees to Plus 450 Degrees F) General Specification for (ASG) |
| MIL-DTL-781 Revision J:2014 | Terminal, Wire Rope Swaging, 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 III 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 |
| 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, General Specification for |
| SAE AS5440A | Hydraulic Systems, Military Aircraft, Design and Installation, Requirements For |
| MIL-HDBK-454 Revision B:2007 | General Guidelines for Electronic Equipment |
| SAE ARP4493A | Aerospace - Direct Drive Servovalves |
| MIL E 5400 : T | ELECTRONIC EQUIPMENT, AEROSPACE, GENERAL SPECIFICATION FOR |
| MIL-STD-7080 Base Document:1994 | Selection and Installation of Aircraft Electric Equipment |
| SAE ARP4761 | GUIDELINES AND METHODS FOR CONDUCTING THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT |
| MIL-STD-464 Revision C:2010 | Electromagnetic Environmental Effects Requirements for Systems |
| SAE AS7997 | 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 (See Notice 2 for Replacement Information) |
| 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 |
| 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 AS94900 | 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 AS35411C | Fittings, Lubrication |
| MIL-S-8512 Revision D:1974 | Support Equipment, Aeronautical, Special, General Specification for the Design of |
| SAE AS50881F | 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 |
| MIL-HDBK-838 Base Document:1997 | Lubrication of Military Equipment |
| SAE ARP4386C | 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 I |
| MIL-STD-202 Revision H:2015 | Electronic and Electrical Component Parts |
| SAE ARP4058A | Actuators: Mechanical, Geared Rotary, General Specification For |
| MIL-HDBK-336-1 Base Document:1982 | Survivability, Aircraft, Nonnuclear, General Criteria-Volume 1 (See Notice 2 for Replacement Information) |
| MIL-HDBK-516 Revision C:2014 | Airworthiness Certification Criteria |
| MIL-HDBK-336-3 Base Document:1983 | Survivability, Aircraft, Nonnuclear, Engine-Volume 3 (See Notice 2 for Replacement Information) |
| MIL-HDBK-2069 Base Document:1997 | Aircraft Survivability |
| SAE ARP490F | Electrohydraulic Servovalves |
| JSSG-2006 Base Document:1998 | Aircraft Structures |
| 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 Bus |
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