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Integrated Rudder and Brake Pedal Unit, General Requirements for Fly-By Wire Transport and Business Aircraft

A-6A3 Flight Control and Vehicle Management Systems Cmt
  • Aerospace Standard
  • ARP6252
  • Current
Published 2018-10-15 by SAE International in United States
This Aerospace Recommended Practice (ARP) provides general requirements for a generic, integrated rudder and brake pedal unit, incorporating a passive force-feel system that could be used for fixed-wing fly-by wire transport and business aircraft. This ARP addresses the following: The functions to be implemented The mechanical interconnection between captain and F/O station The geometric and mechanical characteristics The mechanical, electrical, and electronic interfaces The safety and certification requirements
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Aerospace - Passive Side Stick Unit General Requirements for Fly by Wire Transport and Business

A-6A3 Flight Control and Vehicle Management Systems Cmt
  • Aerospace Standard
  • ARP6001A
  • Current
Published 2018-10-04 by SAE International in United States
This SAE Aerospace Recommended Practice (ARP) provides general requirements for a generic “passive” side stick that could be used for fly by wire transport and business aircraft. It addresses the following: The functions to be implemented The geometric and mechanical characteristics The mechanical and electrical interfaces The safety and certification requirements
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Vehicle Management Systems - Flight Control Function, Design, Installation and Test of Piloted Military Aircraft, General Specification For

A-6A3 Flight Control and Vehicle Management Systems Cmt
  • Aerospace Standard
  • AS94900A
  • Current
Published 2018-08-13 by SAE International in United States
This SAE Aerospace Standard (AS) provides the general performance, design, installation, test, development, and quality assurance requirements for the flight control related functions of the Vehicle Management Systems (VMS) of military piloted aircraft. It also provides specification guidance for the flight control interfaces with other systems and subsystems of the aircraft.
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Description of Actuation Systems for Aircraft With Fly-By-Wire Flight Control Systems

A-6A3 Flight Control and Vehicle Management Systems Cmt
  • Aerospace Standard
  • AIR4253B
  • Current
Published 2018-07-24 by SAE International in United States
This SAE Aerospace Information Report (AIR) provides design information of various contemporary aircraft fly-by-wire (FBW) flight control actuation systems that may be useful in the design of future systems for similar applications. It is primarily applicable to manned aircraft. It presents the basic characteristics, hardware descriptions, redundancy concepts, functional schematics, and discussions of the servo controls, failure monitoring, and fault tolerance. All existing FBW actuation systems are not described herein; however, those most representing the latest designs are included. While this AIR is intended as a reference source of information for aircraft actuation system designs, the exclusion or omission of any other appropriate actuation system or subsystem should not limit consideration of their use on future aircraft.
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Aerospace Active Inceptor Systems for Aircraft Flight and Engine Controls

A-6A3 Flight Control and Vehicle Management Systems Cmt
  • Aerospace Standard
  • ARP5764
  • Current
Published 2018-07-24 by SAE International in United States
The purpose of this document is to develop the general characteristics and requirements for feel-force control systems for active cockpit controllers, also known as Active Inceptors. The document presents technical material that describes the recommended key characteristics and design considerations for these types of systems. Where appropriate, the effects of platform specific requirements (e.g., single axis/dual axis, single seat/dual seat, civil/military, rotorcraft/fixed wing aircraft, etc.) are clearly identified. The material developed will serve as a reference guide for: a Aircraft prime contractors who want to understand active cockpit controller technology and develop their own set of requirements; b Suppliers that develop active cockpit controller equipment and; c Regulatory Authorities who will be involved in the certification of these types of systems.
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Validation and Verification Process Steps for Monitors Development in Complex Flight Control and Related Systems

A-6A3 Flight Control and Vehicle Management Systems Cmt
  • Aerospace Standard
  • ARP6539
  • Current
Published 2017-11-30 by SAE International in United States
This SAE Aerospace Recommended Practice (ARP) provides a process for the verification and validation of monitors used in highly-integrated and complex aircraft flight control and related systems.
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Aircraft Flight Control Systems Descriptions

A-6A3 Flight Control and Vehicle Management Systems Cmt
  • Aerospace Standard
  • AIR4094A
  • Current
Published 2016-07-18 by SAE International in United States
This SAE Aerospace Information Report (AIR) supplies information on the flight control systems incorporated on various current and historic fixed wing, rotary wing, and tilt rotor aircraft. A brief description of the aircraft is followed by a description of the flight control system, some specific components, drawings of the internal arrangement, block diagrams, and schematics. System operation redundancy management is also presented.
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Primary Flight Control Hydraulic Actuation System Interface Definition

A-6A3 Flight Control and Vehicle Management Systems Cmt
  • Aerospace Standard
  • AIR4922A
  • Current
Published 2015-10-19 by SAE International in United States
This SAE Aerospace Information Report (AIR) provides a description of the interfaces and their requirements for generic and specific hydraulic actuation systems used in the flight control systems of manned aircraft. Included are the basic control system characteristics and functional requirements, and the essential interfaces (structural, mechanical, hydraulic power, control input, status monitoring, and environment). Major design issues, requirements, and other considerations are presented and discussed.
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Descriptions of Systems Integration Test Rigs (Iron Birds) For Aerospace Applications

A-6A3 Flight Control and Vehicle Management Systems Cmt
  • Aerospace Standard
  • AIR5992
  • Current
Published 2015-10-16 by SAE International in United States
This Aerospace Information Report (AIR) provides information on systems integration rigs, commonly referred to as “Iron Birds” for aerospace applications. a It includes background historical information including descriptions of Iron Birds produced to date, important component elements and selection rationale, hydraulic system design and operational modes and illustrates the design approaches to be considered. b It provides illustrations of the various systems that should be considered for Iron Bird testing in the development phase and utilization during the production program. c It includes recommendations for simulation, component development tests, system integration and lessons learned.
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Aerospace Fly-by-Light Actuation Systems

A-6A3 Flight Control and Vehicle Management Systems Cmt
  • Aerospace Standard
  • AIR4982A
  • Current
Published 2014-12-18 by SAE International in United States
This SAE Aerospace Information Report (AIR) has been prepared to provide information regarding options for optical control of fluid power actuation devices. It is not intended to establish standards for optical fluid power control, but rather is intended to provide a baseline or foundation from which standards can be developed. It presents and discusses approaches for command and communication with the actuation device via electro-optic means. The development of standards will require industry wide participation and cooperation to ensure interface commonality, reliability, and early reduction to practice. To facilitate such participation, this document provides potential users of the technology a balanced consensus on its present state of development, the prospects for demonstration of production readiness, and a discussion of problem areas within this technology. The intent is to inform the user/designer of the options available for interfacing photonics (optics) to hydraulic power control actuators used in aerospace applications. Specifically, power and signal interfaces such as control, status and BIT (built in test) are considered. Mechanical interfaces such as optical connectors and fibers are also discussed.…
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