Airplane complete machine electromagnetic compatible digitalization model system

An electromagnetic compatibility and model system technology, applied in the direction of electrical digital data processing, special data processing applications, instruments, etc., can solve the system-level design that cannot meet the needs of the electromagnetic compatibility design simulation of the whole aircraft, and has no science of electromagnetic compatibility of the aircraft. Complicated circuit functions and structures, etc.
CN101436221AActive Publication Date: 2009-05-20BEIHANG UNIV
0 Cites 33 Cited by

Patent Information

Authority / Receiving Office
CN Β· China
Current Assignee / Owner
BEIHANG UNIV
Publication Date
2009-05-20

Smart Images

  • Figure 1
    Figure 1
  • Figure 2
    Figure 2
  • Figure 3
    Figure 3
Patent Text Reader

Abstract

The invention discloses an electromagnetic compatible digitized model system for a whole aircraft, which comprises an aircraft parameterized surface model construction unit (1), an airborne equipment position matching unit (2), an airborne equipment interference associated unit (3), an electromagnetic environment distribution unit (4) and a sensitive equipment interference source acquisition unit (5). The invention constructs the electromagnetic compatible digitized model system for the whole aircraft by adoption of the behavioral simulation method, application of the 'grey box' theory, consideration of characteristic parameters of electronic airborne equipment from the aspect of system level, neglect of various circuit details, and digitized modeling simulation of the electronic airborne equipment of the aircraft.
Need to check novelty before this filing date? Find Prior Art

Description

technical field

[0001] The present invention relates to the field of electromagnetic compatibility design, and more particularly refers to a digital model system applicable to the aircraft design process, which uses a behavioral simulation method to perform system-level electromagnetic compatibility on the entire aircraft. Background technique

[0002] In the traditional aircraft electromagnetic compatibility design method, the overall design unit of the aircraft proposes performance index requirements for communication, navigation and other airborne electronic equipment based on the performance requirements of the whole aircraft. In the development or production process of airborne electronic equipment, functional requirements are mainly considered. To realize the design parameters, the electromagnetic compatibility interrelationship between the airborne electronic equipment is not fully considered; when the airborne electronic equipment is developed, the electromagnetic com...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More