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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

Inactive Publication Date: 2019-12-31
SHENZHEN AUTEL INTELLIGENT AVIATION TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] Since these devices may be distributed in different operating systems, there may be a system time difference in the scheduling itself, and there is a communication delay between the devices, which will lead to asynchronous sending and receiving time of data information, resulting in the inability to accurately obtain aircraft information. The current state and control the accurate movement of the aircraft

Method used

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  • Aircraft time synchronization system and method

Examples

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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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PUM

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Abstract

The embodiment of the invention discloses an aircraft time synchronization system and method. The system comprises a first communication module and a second communication module, data transmission iscarried out between the first communication module and the second communication module through a communication line, and an I / O interface of the first communication module is connected with an I / O interface of the second communication module through an interrupt signal line; the first communication module sends data information to the second communication module through a communication line, and sends a triggered interrupt signal to the second communication module through an interrupt signal line, wherein the data information comprises sending time when the data information is sent and an interrupt signal is triggered; and the second communication module performs time synchronization with the first communication module based on the determined communication time difference and system time difference with the first communication module according to the data information and the receiving time and sending time of the interrupt signal. Accurate time synchronization among different communication modules of the aircraft is realized, so that the movement of the aircraft is accurately controlled.

Description

technical field [0001] Embodiments of the present invention relate to the technical field of aircraft, and in particular to an aircraft time synchronization system and method. Background technique [0002] With the development of science and technology, the scope of application of aircraft has become wider and wider, ranging from military use at the national level to entertainment use at the personal level. For example, the aircraft may be a drone. Usually, the aircraft includes multiple devices for collecting information such as the current position and attitude information of the aircraft and images of the environment in which it is located. After communication between these devices, motion control instructions are generated to control the subsequent motion state of the aircraft. [0003] Since these devices may be distributed in different operating systems, there may be a system time difference in the scheduling itself, and there is a communication delay between the devi...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H04W56/00H04W4/42H04L7/00H04L29/08
CPCH04W56/001H04W4/42H04L7/00H04L67/12H04W56/0055G06F13/24H04W4/40H04J3/0635
Inventor 李昭早
Owner SHENZHEN AUTEL INTELLIGENT AVIATION TECH CO LTD
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