The Experts below are selected from a list of 300 Experts worldwide ranked by ideXlab platform

E.j. Borgstrom - One of the best experts 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 - One of the best experts on this subject based on the ideXlab platform.

Li Loude - One of the best experts 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.

Donglin Su - One of the best experts on this subject based on the ideXlab platform.

  • Research on radiation emission limits of Airborne Equipment
    2013 5th IEEE International Symposium on Microwave Antenna Propagation and EMC Technologies for Wireless Communications, 2013
    Co-Authors: Nankai Wu, Donglin Su
    Abstract:

    This paper introduces a method of estimating the Airborne Equipment radiation interference and calculating radiation emission limit. According to the uniqueness theorem of electromagnetic field, the model of the radiation source are described, which is theoretically proved that it is equivalent to the radiation source. The method is present with a practical engineering example,which establish a platform model and equivalent source model. Combined with microwave network theory and numerical simulation software, the radiation interference to the shortwave radio receiver is predicted. In order to satisfy the compatibility of shortwave radio receiver, the radiation emission limit of the interference source is calculated. Finally, the process and method of the equivalent source model of tailoring radiation emission limit is summarized; which can help the engineering set the emission limit and unsure the compatibility of the near-by Airborne Equipment.

  • The complex network model of the Airborne Equipment electromagnetic compatibility
    Proceedings of the 9th International Symposium on Antennas Propagation and EM Theory, 2010
    Co-Authors: Guo Dandan, Donglin Su, Xie Yongjun, Wu Longgang, Zhao Xiaoying
    Abstract:

    First of all, this paper analyzes the electromagnetic compatibility characteristics of Airborne Equipment system, and based on that, this paper presents ideas that the Airborne Equipment system could be networks. Second, in accordance with the actual situation, this paper proposes an AEMC network which reflects the electromagnetic relationship among the aircraft Equipment with multi-nodes, directed multi-edges and double-layers. And then, this paper analyzes the AEMC network evolution by simulate methods, the AEMC network has two behaviors: the small-world and the scale-free. The small-world indicates that interference signal of Airborne Equipment system is easy to spread; the scale-free indicates the existence of the key Equipments which affects Airborne Equipment electromagnetic compatibility.

Li Xiao-ming - One of the best experts on this subject based on the ideXlab platform.