Method for debugging operating software of aircraft onboard system and equipment for implementing the method
A technology for running software and airborne systems, which is applied in the field of systems with high security requirements, and can solve problems such as disappearance and reverse execution efficiency reduction
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[0094] In step 41, the reverse execution of the function that allows the detected defective instruction string to be traced back to the program is started. In one embodiment of the present invention, the reverse execution is completed between two consecutive marks (interval). In the most common case this corresponds to the start and end of the defect function. It is of course possible to jump from one interval to another without any special restrictions. In another specific embodiment, the reverse execution is carried out over a narrow range around the error, in other words only over a part of the function.
[0095] In step 42 , the developer performs error debugging, in other words he detects errors in defective function sections and corrects them. When the debugging step 42 ends, the method repeats step 31 in order to check whether the program was executed correctly.
[0096] When the control unit no longer detects interrupts on processor exceptions, the control unit then...
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