Integrated electronic system simulation device of a general-purpose aircraft
A simulation device and electronic system technology, which is applied in the fields of electrical digital data processing, special data processing applications, instruments, etc., can solve problems such as the growth of the development cycle and the adverse effects of aircraft development projects, so as to reduce the development cost, control the development risk, shorten the The effect of the development cycle
Pending Publication Date: 2019-06-11
R&D INST OF CHINA AVIATION IND GENERAL AIRCRAFT
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Problems solved by technology
[0003] The demand for integration has brought higher requirements to the development and integration of airborne electronic systems, which has increased the risk of development, and may increase the development cycle, which has a negative impact on aircraft development projects
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[0019] The technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some of the embodiments of the present invention, not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.
[0020] The invention provides an integrated electronic system simulation device for 23 general aircrafts. as attached figure 1 As shown in , the simulation device includes: simulation control 101 , integrated display and control simulation 102 , model simulation 103 , model dynamic excitation 104 and visual scene 105 . The simulation control 101 is respectively connected with the model simulation 103, the model dynamic excitation 104 and the visual sce...
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The invention discloses an integrated electronic system simulation device of a general aircraft. The integrated electronic system simulation device is characterized in that simulation control (101) completes work control of initialization, starting, stopping, dynamic parameter adjustment and mode switching of model simulation (103), model dynamic excitation (104) and a view (105); the comprehensive display control simulation (102) completes display pictures and logic of a comprehensive display, and completes simulation of a control panel of the communication, navigation and indication recording system at the same time; the model simulation (103) is used for simulating equipment or modules of an avionics and electromechanical system; wherein the model dynamic excitation (104) completes thedynamic excitation of the model simulation (103). By the adoption of the method, the dynamic digital simulation problem of developing a general aircraft integrated electronic system can be solved, thedevelopment cycle can be greatly shortened, the development cost can be greatly reduced, meanwhile, multi-wheel design iteration can be supported, the maturity of newly-researched products can be improved, and therefore the development risk can be well controlled.
Description
technical field [0001] The invention relates to the technical field of integrated electronic systems of general aircrafts, in particular to an integrated electronic system simulation device for 23 general aircrafts. Background technique [0002] General-purpose aircraft includes both non-civil aviation passenger aircraft of Part 25 and all aircraft of Part 23, as well as light sports aircraft and experimental aircraft made by flying enthusiasts. Among them, the 23 general-purpose aircraft are important members of the general-purpose aircraft family in terms of quantity and type. There are many types and large differences in configuration, resulting in great differences in the on-board electronic systems. Due to the requirements of aircraft space and load, the The volume and weight of airborne equipment are very high. With the development of electronic technology, integrated electronic system has become the development trend of this type of aircraft airborne electronic system...
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Inventor 赵红军蔡志勇石磊刘斌刘燕龙
Owner R&D INST OF CHINA AVIATION IND GENERAL AIRCRAFT