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Human Factor Considerations in the Implementation of IVHM

HM-1 Integrated Vehicle Health Management Committee
  • Aerospace Standard
  • AIR6915
  • Current
Published 2020-03-20 by SAE International in United States
This SAE Aerospace Information Report (AIR) offers information on how human factors should be considered when developing and implementing IVHM capabilities for both military and civil fixed wing aircraft. These considerations will cover the perception, analysis, and action taken by the flight crew and the maintenance personnel in response to outputs from the IVHM system. These outputs would be onboard realtime for the flight crew and post flight for maintenance. This document is not intended to be a guideline; it is intended to provide information that should be considered when designing and implementing future IVHM systems.
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Control Measures for Laser Safety in the Navigable Airspace

G10T Laser Safety Hazards Committee
  • Aerospace Standard
  • ARP5572A
  • Current
Published 2020-03-10 by SAE International in United States
This SAE Aerospace Recommended Practice (ARP) provides information and guidance for the control of hazardous laser energy in the navigable airspace. This ARP does not address techniqies that pilots can apply to mitigate laser illuminations during a critical phase of flight. Such mitigation strategies are described in ARP6378.
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Electronic Engine Control Design Guide for Electromagnetic Environmental Effects

E-36 Electronic Engine Controls Committee
  • Aerospace Standard
  • AIR5060B
  • Current
Published 2020-02-26 by SAE International in United States
The purpose of this document is to provide reference material for establishing compatibility of electronic gas turbine engine control systems and associated components with the electromagnetic environment and achieving compliance with associated airworthiness requirements.
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Aircraft Instrument and Instrument System Standards: Wording Terminology, Phraseology, Environment and Design Standards For

A-4 Aircraft Instruments Committee
  • Aerospace Standard
  • AIR818E
  • Current
Published 2020-02-20 by SAE International in United States
This Aerospace Standard, (AS), specifies minimum performance standards for _____________ (Instrument or instrument systems) which are primarily intended for use with (vehicles capable of flight), ((fixed wing, rotary wing) aircraft)), (other special modifiers); (and whose purpose is to display _____________ information).
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Ice and Rain Minimum Qualification Standards for Pitot and Pitot-static Probes

AC-9C Aircraft Icing Technology Committee
  • Aerospace Standard
  • AS5562
  • Current
Published 2020-02-11 by SAE International in United States
This SAE Aerospace Standard (AS) establishes minimum ice and rain performance criteria for electrically-heated pitot and pitot-static probes intended for use on the following classes of fixed-wing aircraft and rotorcraft. The classes of fixed-wing aircraft are defined by aircraft flight envelopes and are shown in Figure 1. The flight envelopes generally fall into the classes as shown below: The user of this standard must evaluate the aircraft level installation requirements for the probe against the class definition criteria to ensure adequate coverage for the application. It may be necessary to step up in class or modify the test conditions in order to meet the applicable installation requirements. NOTE: Class 2 is divided into two subgroups identified as either Class 2a or Class 2b. Class 2a probe applications typically include aircraft that operate within the mid to lower end of the Class 2 altitude range and that only use probe output to display basic airspeed and/or altitude. As such, Class 2a probes do not have to test ice crystals at an altitude-capable icing tunnel. Class 2b…
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Passive RFID Tags Intended for Airborne Equipment Use

G-18 Radio Frequency Identification (RFID) Aero Applications
  • Aerospace Standard
  • AS5678B
  • Current
Published 2020-02-05 by SAE International in United States
The scope of this document is to: 1 Provide a requirements document for RFID tag manufacturers to produce passive-only UHF RFID tags for the aerospace industry. 2 Identify the minimum performance requirements specific to the Passive UHF RFID Tag to be used on airborne equipment, to be accessed only during ground operations. 3 Specify the test requirements specific to Passive UHF RFID tags for airborne equipment use, in addition to EUROCAE ED-14 / RTCA DO-160 compliance requirements separately called out in this document. 4 Identify existing standards applicable to Passive UHF RFID Tag. 5 Provide a certification standard for RFID tags which will use permanently-affixed installation on airborne equipment.
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Adding Context to Full-Motion Video for Improved Surveillance and Situational Awareness

  • Magazine Article
  • TBMG-36055
Published 2020-02-01 by Tech Briefs Media Group in United States

Today’s intelligence, surveillance, and reconnaissance (ISR) platforms integrate state-of-the-art technologies and subsystems into airborne platforms intended to observe, detect, identify, and neutralize threats. Full motion video (FMV) sensors are essential assets and are routinely used on fixed-wing, rotary-wing, and manned and unmanned platforms to provide real-time situational awareness with minimal latency.

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Adding Context to Full-Motion Video for Improved Surveillance and Situational Awareness

Aerospace & Defense Technology: February 2020

  • Magazine Article
  • 20AERP02_03
Published 2020-02-01 by SAE International in United States

Today's intelligence, surveillance, and reconnaissance (ISR) platforms integrate state-of-the-art technologies and subsystems into airborne platforms intended to observe, detect, identify, and neutralize threats. Full motion video (FMV) sensors are essential assets and are routinely used on fixed-wing, rotary-wing, and manned and unmanned platforms to provide real-time situational awareness with minimal latency.

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Specification Guide for Power Drive Units (PDUs)

A-6B3 Electro-Mechanical Actuation Committee
  • Aerospace Standard
  • ARP5384
  • Current
Published 2020-01-06 by SAE International in United States
This Recommended Practice provides a guide for specifying general design, performance, and test requirements for power drive units (PDUs) for flight controls and other applications.
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Lighting Applications for Unmanned Aircraft Systems (UAS)

A-20B Exterior Lighting Committee
  • Aerospace Standard
  • ARP6336
  • Current
Published 2019-12-05 by SAE International in United States
This SAE Aerospace Recommended Practice (ARP) provides technical recommendations for the lighting applications for Unmanned Aircraft Systems (UAS). The technical content of this ARP discusses the unique trade-offs that are necessary to maintain commonality to the U.S. Federal Aviation Regulations (FARs)1 for aerospace lighting. The recommendations set forth in this document are to aid in the design of Unmanned Aircraft (UA) lighting for the size of aircraft and operation for which the aircraft is intended. In addition, certain concepts of operation for which UASs are suited will require unique lighting solutions.
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