Aircraft time synchronization system and method
A time synchronization system and time synchronization technology, which is applied in the field of aircraft, can solve the problems of system time difference, out-of-synchronization of sending and receiving time of data information, inability to accurately obtain the current state of the aircraft, etc., and achieve the effect of precise time synchronization
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Embodiment 1
[0019] figure 1 It is a schematic diagram of an aircraft time synchronization system provided by Embodiment 1 of the present invention. This embodiment is applicable to the case of time synchronization of different communication modules in an aircraft. The system specifically includes:
[0020] The first communication module 102 and the second communication module 104, between the first communication module 102 and the second communication module 104 carry out data transmission through the communication line 106, the I / O interface 110 of the first communication module 102 communicates with the interrupt signal line 108 The I / O interface 110 of the second communication module 104 is connected.
[0021] Wherein, the first communication module 102 and the second communication module 104 are two different communication modules in the same aircraft, and the first communication module 102 and the second communication module 104 may be distributed in different operating systems. The...
Embodiment 2
[0037] Figure 2a A schematic diagram of an aircraft time synchronization system provided in Embodiment 2 of the present invention, as shown in Figure 2a As shown, a specific example is used for illustration.
[0038]Optionally, the aircraft may include an aircraft control module 202 and a vision processing module 204 . Data transmission is performed between the aircraft control module 202 and the vision processing module 204 through the communication line 106 , and the I / O interface 110 of the aircraft control module 202 is connected to the I / O interface 110 of the vision processing module 204 through the interrupt signal line 108 .
[0039] Specifically, the first communication module 102 can be the aircraft control module 202, the second communication module 104 can be the vision processing module 204, and the aircraft control module 202 can collect the position and attitude information of the aircraft, that is, the pose information, through the communication line 106 is...
Embodiment 3
[0068] image 3 It is a flow chart of an aircraft time synchronization method in Embodiment 3 of the present invention, which can be executed based on the aircraft time synchronization system provided in the above embodiments, such as image 3 As shown, the aircraft time synchronization method includes:
[0069] Step 312: Receive the data information and the interrupt signal sent by the first communication module; wherein, the data information includes the sending time when the data information is sent and the interrupt signal is triggered.
[0070] Optionally, the first communication module sends data information to the second communication module through the communication line, and at the same time sends the triggered interrupt signal to the second communication module through the interrupt signal line.
[0071] Optionally, data transmission is performed between the first communication module and the second communication module through a communication line, and the I / O inte...
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