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Airborne Equipment

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E.j. Borgstrom – 1st expert on this subject based on the ideXlab platform

  • A comparison of methods and results using the semi-anechoic and reverberation chamber radiated RF susceptibility test procedures in RTCA/DO-160D, Change One
    2002 IEEE International Symposium on Electromagnetic Compatibility, 2002
    Co-Authors: E.j. Borgstrom

    Abstract:

    RTCA/DO-160D, Environmental Conditions and Test Procedures for Airborne Equipment, defines a series of minimum standard environmental and electromagnetic compatibility test conditions (categories) and applicable laboratory test procedures for Airborne Equipment. Change One, issued in December, 2000, includes a complete revision of Section 20- Radio Frequency Susceptibility (Radiated and Conducted), which contains two different radiated RF susceptibility test procedures: reverberation chamber (which was extensively changed), and semi-anechoic chamber (which was updated). This paper provides a comparison of the two procedures, including chamber specifications, test setups, calibration methods, and test procedures. A comparison of radiated susceptibility test results using both methods is also discussed.

  • Radio frequency susceptibility testing for RTCA/DO-160D, after change notice one
    Gateway to the New Millennium. 18th Digital Avionics Systems Conference. Proceedings (Cat. No.99CH37033), 1999
    Co-Authors: E.j. Borgstrom

    Abstract:

    RTCA/DO-160D, Environmental Conditions and Test Procedures for Airborne Equipment, defines a series of minimum standard environmental test conditions (categories) and applicable test procedures for Airborne Equipment. The purpose of these tests is to provide a laboratory means of determining the performance characteristics of Airborne Equipment in environmental conditions representative of those which may be encountered in Airborne operation of the Equipment. This paper is a follow-up to the paper covering DO-160D given by the author at the 1998 DASC, and provides a detailed description of the Radio Frequency susceptibility requirements in Change Notice One for Section 20 of RTCA/DO-160D. Background and rationale for the changes in Section 20 are also discussed from the author’s perspective as a member of RTCA/Special Committee 135, Working Group 20 (WG-20), which is responsible for producing Change Notice One for DO-160D, Section 20.

  • An overview of the EMC requirements in RTCA/DO-160D
    1998 IEEE EMC Symposium. International Symposium on Electromagnetic Compatibility. Symposium Record (Cat. No.98CH36253), 1998
    Co-Authors: E.j. Borgstrom

    Abstract:

    RTC/DO-160D, Environmental Conditions and Test Procedures for Airborne Equipment, defines a series of minimum standard environmental test conditions (categories) and applicable test procedures for Airborne Equipment. The purpose of these tests is to provide a laboratory means of determining the performance characteristics of Airborne Equipment in environmental conditions representative of those which may be encountered in Airborne operation of the Equipment. This paper provides an overview of the electromagnetic compatibility requirements in RTCA/DO-160D. Future directions and changes to DO-160D is also discussed from the author’s perspective as a member of RTCA/Special Committee 135, which is responsible for producing DO-160D.

Li Hong-lie – 2nd expert on this subject based on the ideXlab platform

  • Designs and Analysis for Electro Magnetic Compatibility on Improvement of Airborne Electrical Equipment
    Aircraft Design, 2020
    Co-Authors: Li Hong-lie

    Abstract:

    According to the real circumstances of the improvement of Airborne Equipment,and the experience of one specific searching and guiding aircraft,interference factors of Airborne Equipment were analyzed,and the electro magnetic compatibility of the Airborne Equipment were designed and analyzed.

Li Loude – 3rd expert on this subject based on the ideXlab platform

  • EMEIT – The design of Airborne Equipment environmental test system based on C
    Proceedings of 2011 International Conference on Electronic & Mechanical Engineering and Information Technology, 2011
    Co-Authors: Li Loude, Yuan Hong-jie

    Abstract:

    This paper introduces the environmental analysis systemof Airborne Equipment and its design process based on Visual Studio 2005. Through reference the design of environment experiments in GJB150 and GJB150A, to analyze the environmental factor of the missiles life period and to design the environments testing conditions. It makes a complete analysis of the environmental factors of the Airborne Equipment lifetime, and gives related tailor to environment test. In addition, it designs test order and test conditions. Finally, it generates the reports of environmental analysis systemof Airborne Equipment and environmental test conditions of Airborne Equipment. This study is useful for engineering application.

  • The design of Airborne Equipment environmental test system based on C#
    Proceedings of 2011 International Conference on Electronic & Mechanical Engineering and Information Technology, 2011
    Co-Authors: Li Loude, Yuan Hongjie

    Abstract:

    This paper introduces the environmental analysis system of Airborne Equipment and its design process based on Visual Studio 2005. Through reference the design of environment experiments in GJB150 and GJB150A, to analyze the environmental factor of the missiles life period and to design the environments testing conditions. It makes a complete analysis of the environmental factors of the Airborne Equipment lifetime, and gives related tailor to environment test. In addition, it designs test order and test conditions. Finally, it generates the reports of environmental analysis systemof Airborne Equipment and environmental test conditions of Airborne Equipment. This study is useful for engineering application.