Monitoring method of emission vehicle states and device
A monitoring device and a technology for launching vehicles, which are applied in the field of launching vehicles, can solve the problems of single function and low security, and achieve the effects of reducing processor consumption, preventing data loss, and saving the overhead of occupying processors.
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Embodiment 1
[0055] Such as Figure 1 to Figure 4 As shown, the present invention discloses a method for monitoring the status of a launch vehicle, which is implemented by five threads. The five threads include a main process, a data receiving process, a data storage process, a data refresh process, and a timer process. Used to display status data and analysis results, the data receiving process is used to obtain data from the CAN bus, the data storage process is used to store the obtained data, the data refresh process is used to update the data displayed on each monitoring interface, and the timer process Used to control the operating cycle of each process.
[0056] Specifically, the monitoring method of the launch vehicle turntable of the present invention includes the following steps:
[0057] Step 1. Before starting the data receiving thread, the monitoring method includes the step of starting the timer thread. The timer thread is used to set the running period of the data receiving thread...
Embodiment 2
[0071] Such as Figure 2 to Figure 4 As shown, corresponding to the aforementioned method for monitoring the state of the launch vehicle, the present invention also discloses a monitoring device for the state of the launch vehicle. The monitoring device includes a data acquisition module, a data upload module, a data display module, a data storage module, and a data analysis. Module and cycle setting module. Such as Figure 4 As shown, the device for monitoring the status of the launch vehicle of the present invention can be integrated in a status detector, which is connected to the first CAN bus and the second CAN bus, and the acquisition box monitors the status of each node on the two CAN buses; , The vehicle control unit, motor control unit, main control unit, main valve box control unit, gateway unit and acquisition unit are the control units on the vehicle control system of the launch vehicle. The main control unit is used to control other control units. The control unit ...
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