Method for generating multistage task system fault physical simulation sections of avionic devices
A technology for avionics equipment and physical simulation, applied in design optimization/simulation, electrical digital data processing, special data processing applications, etc.
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[0023] The present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments.
[0024] The following takes an aircraft inertial navigation system as an example to illustrate its reliability profile generation process based on fault physics.
[0025] The invention provides a method for generating a reliability simulation profile of avionics equipment based on fault physics. figure 1 A schematic diagram of the workflow of the present invention is shown. In this embodiment, the specific steps of the method are as follows:
[0026] Step 1: Determine the tasks of the aircraft where the inertial navigation system is located at different stages.
[0027] The aircraft performs two missions a day, outbound and return. According to the working condition table of the flight mission, each flight mission is shown in Table 1, including the following processes: shutdown (that is, all equipment is in the off state), ground idle, groun...
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