CN208188215U - Aircraft ground Auto-Test System based on Real Time Serial Communication - Google Patents

Abstract

Aircraft ground automatic test system based on real-time serial communication, involving the field of aircraft measurement and control technology; including power management module, power supply control relay module, signal conditioning module, analog quantity acquisition module, digital acquisition module, communication module, upper computer module and lower computer Module; the utility model adopts a highly integrated design, through the integration of many general interfaces, according to the data communication relationship between multiple devices, and through the reasonable design of the test sequence of the test method, a test process is covered to multiple devices, effectively The number of devices covered by a single test is increased; multiple devices are cross-linked at the same time and tested in parallel. Start the automatic test process, and the test system will be gradually launched during the test. During this period, no manual intervention is required. The test results can be judged intuitively by the program, which effectively reduces the manual workload.

Description

Aircraft Ground Automatic Test System Based on Real-time Serial Communication

technical field

The utility model relates to the technical field of aircraft measurement and control, in particular to an aircraft ground automatic test system based on real-time serial communication.

Background technique

The ground test of the aircraft requires high efficiency, that is, to simplify the ground test workflow on the basis of reliability, shorten the preparation time, and ensure the comprehensiveness and accuracy of the test. Especially in wartime, when it is necessary to ensure the rapid deployment of tactics and the rapid launch of missiles, the high-efficiency test of aircraft is very important.

At present, aircraft testing needs to go through the following tests: individual testing of airborne or missile-borne equipment, final assembly integration testing, and simulation testing. Throughout the testing process, the main problems are as follows:

(1) The test coverage of the test method is low, and the test of airborne or missile-borne equipment often only depends on their own independent test tools. Before the final assembly of the equipment, the operator uses the independent test of each equipment to test one by one, which will result in a large number of on-site equipment, and the operations required to complete all the test items are extremely cumbersome.

(2) The test efficiency is low, especially when it comes to equipment cross-linking, it is difficult to implement with a single equipment. Taking the electronic control box as an example, the test of this device often requires multiple digital output channels, which are tested by the manufacturer before leaving the factory. When the final assembly is delivered, the user often does not have the test conditions, but it can be quickly checked by connecting with the flight control device. Testing for functionality, which involves device crosslinking, for which there are few tools or methods available.

(3) Multifunctional testing often requires a lot of hardware accumulation. Conventional test methods need to accumulate a lot of hardware resources in order to complete the test of various modes, such as upper and lower computers, real-time systems, and communication design among various hardware. With the increase of test items, the design of the system will become more complex.

Utility model content

The purpose of the utility model is to overcome the above-mentioned shortcomings of the prior art, provide an aircraft ground automatic test system based on real-time serial communication, and solve the problems of low test coverage, low test efficiency, and hardware accumulation during multi-function tests.

The above-mentioned purpose of the utility model is achieved through the following technical solutions:

Aircraft ground automatic test system based on real-time serial communication, including power management module, power supply control relay module, signal conditioning module, analog quantity acquisition module, digital acquisition module, communication module, upper computer module and lower computer module;

Power management module: receives the AC power from the external power supply system, and transmits the AC power to the power supply control relay module;

Power supply control relay module: receive the AC power from the power management module, and supply power to the external equipment under test;

Analog quantity acquisition module: collect the analog quantity signal of voltage and current of the external device under test, and send the analog quantity signal of voltage and current to the signal conditioning module;

Digital acquisition module: collect the connected or disconnected state of the external device under test and the external power supply box; convert the connected or disconnected state into a connected or disconnected digital signal, and send the connected or disconnected digital signal to the signal conditioning module;

Signal Conditioning Module: Receive analog signals of voltage and current from the analog acquisition module; amplify and filter the analog signals of voltage and current in turn, generate filtered and amplified voltage and current signals, and filter and amplify them Send the voltage and current signals to the upper computer module; receive the connected or disconnected digital signal from the digital acquisition module; convert the connected or disconnected digital signal into a connected or disconnected electrical signal; and send the connected or disconnected electrical signal To the host computer module;

Communication module: collect the status information of the external device under test, and send the status information of the external device under test to the upper computer module and the lower computer module;

Host computer module: Receive the filtered and amplified voltage and current signals from the signal conditioning module; receive the connection or disconnection electrical signal from the signal conditioning module; receive the status of the external device under test from the communication module or the lower computer module Information; store, display and monitor the filtered and amplified voltage and current signals, connect or disconnect electrical signals, and the status information of external equipment to be tested; send the control signal of the lower computer to the lower computer module to realize the control of the lower computer module control;

Lower computer module: Receive the status information of the external device under test from the communication module; send the status information of the external device under test to the upper computer module; receive the lower computer control signal from the upper computer; generate the control command of the external device under test ; and send the control command of the external device under test to the external device under test through the communication module, so as to realize the control of the external device under test.

In the above-mentioned automatic ground test system for aircraft based on real-time serial communication, the AC power transmitted from the external power supply system is 220V.

In the above-mentioned aircraft ground automatic test system based on real-time serial communication, when the signal conditioning module receives the connected digital signal from the digital acquisition module, it converts the connected digital signal into a 5V electrical signal, and sends the 5V electrical signal to the host computer module.

In the above-mentioned aircraft ground automatic test system based on real-time serial communication, when the signal conditioning module receives the disconnected digital signal from the digital acquisition module, it converts the disconnected digital signal into a 0V electrical signal, and sends the 0V electrical signal to PC module.

In the above-mentioned automatic ground test system for aircraft based on real-time serial communication, the status information of the external equipment to be tested includes on-board navigation data and on-board device status data.

In the above-mentioned aircraft ground automatic test system based on real-time serial communication, when the status information of the external device to be tested is sent and received in real time, the communication module first sends the status information of the external device to be tested to the lower computer module; and the lower computer module Send the status information of the external device under test to the host computer module; when the status information of the external device under test is not real-time sending and receiving, the communication module directly sends the status information of the external device under test to the host computer module.

In the above-mentioned automatic ground test system for aircraft based on real-time serial communication, the control signal of the lower computer includes start, stop and reset control signals for the lower computer.

In the aforementioned real-time serial communication-based aircraft ground automatic test system, the external device-under-test control instructions include navigation data control instructions and device-under-test control instructions.

Compared with the prior art, the utility model has the following advantages:

(1) The utility model adopts a highly integrated design, by integrating many common interfaces, according to the data communication relationship between multiple devices, and by rationally designing the test sequence of the test method, one test process is covered by multiple devices, effectively Greatly increased the number of devices covered by a single test;

(2) The utility model cross-links multiple devices and tests them in parallel. Start the automatic test process, and the test system will be gradually launched during the test. During this period, no manual intervention is required. The test results can be judged intuitively by the program, which effectively reduces the manual workload.

Description of drawings

Fig. 1 is the block diagram of the utility model automatic test system.

Detailed ways

Below in conjunction with accompanying drawing and specific embodiment the utility model is described in further detail:

The utility model is an aircraft ground automatic test system based on real-time serial communication. The upper computer test management software executes the foreground program, including non-real-time tasks such as data monitoring, display and storage; the lower computer executes the real-time test process by the exclusive kernel thread based on the RTX real-time driver, and the background real-time program of the lower computer runs independently without any External interrupt intervention. The upper computer obtains the data of the lower computer from the data memory area through the lower computer operation class.

As shown in Figure 1, it is a block diagram of the automatic test system. It can be seen from the figure that the aircraft ground automatic test system based on real-time serial communication includes a power management module, a power supply control relay module, a signal conditioning module, an analog acquisition module, a digital acquisition module, Communication module, upper computer module and lower computer module.

Power management module: receives 220V AC from the external power supply system, and transmits the AC to the power supply control relay module.

Power supply control relay module: receive the AC power from the power management module, and supply power to the external device under test.

Analog quantity acquisition module: collect the analog quantity signals of the voltage and current of the external device under test, and send the analog quantity signals of the voltage and current to the signal conditioning module.

Digital acquisition module: collect the connected or disconnected state of the external device under test and the external power supply box; convert the connected or disconnected state into a connected or disconnected digital signal, and send the connected or disconnected digital signal to the signal conditioning module.

Signal Conditioning Module: Receive analog signals of voltage and current from the analog acquisition module; amplify and filter the analog signals of voltage and current in turn, generate filtered and amplified voltage and current signals, and filter and amplify them Send the voltage and current signals to the upper computer module; receive the connected or disconnected digital signal from the digital acquisition module; convert the connected or disconnected digital signal into a connected or disconnected electrical signal; when the signal conditioning module receives the digital acquisition module When the digital signal is connected, it converts the connected digital signal into a 5V electrical signal, and sends the 5V electrical signal to the host computer module; when the signal conditioning module receives the disconnected digital signal from the digital acquisition module, it disconnects the digital signal Convert it into a 0V electrical signal, and send the 0V electrical signal to the host computer module.

Communication module: collect the status information of the external device under test, the status information of the external device under test includes the navigation data on the bomb and the status data of the device on the bomb; and send the status information of the external device under test to the upper computer module and the lower computer module.

Host computer module: Receive the filtered and amplified voltage and current signals from the signal conditioning module; receive the connection or disconnection electrical signal from the signal conditioning module; receive the status of the external device under test from the communication module or the lower computer module Information; store, display and monitor the filtered and amplified voltage and current signals, connect or disconnect electrical signals, and the status information of external equipment to be tested; send the control signal of the lower computer to the lower computer module to realize the control of the lower computer module control.

Lower computer module: Receive the status information of the external device under test from the communication module; send the status information of the external device under test to the upper computer module; receive the lower computer control signal from the upper computer; the lower computer control signal includes Machine start, stop and reset control signals. Generate an external device under test control command; the external device under test control command includes a navigation data control command and a device under test control command. And the control command of the external device under test is sent to the external device under test through the communication module, so as to realize the control of the external device under test.

When the status information of the external device under test is sent and received in real time, the communication module first sends the status information of the external device under test to the lower computer module; and the lower computer module sends the status information of the external device under test to the upper computer module; When the state information of the external device under test is not real-time sending and receiving, the communication module directly sends the state information of the external device under test to the host computer module.

During the entire test process, the foreground program executed by the host computer test management software can intuitively observe the status of each device under test.

The content that is not described in detail in the description of the utility model belongs to the known technology of those skilled in the art.

Claims (8)

1. The aircraft ground automatic test system based on real-time serial communication is characterized in that: comprising a power management module, a power supply control relay module, a signal conditioning module, an analog quantity acquisition module, a digital acquisition module, a communication module, an upper computer module and a lower computer module; Power management module: receives the AC power from the external power supply system, and transmits the AC power to the power supply control relay module; Power supply control relay module: receive the AC power from the power management module, and supply power to the external equipment under test; Analog quantity acquisition module: collect the analog quantity signal of voltage and current of the external device under test, and send the analog quantity signal of voltage and current to the signal conditioning module; Digital acquisition module: collect the connected or disconnected state of the external device under test and the external power supply box; convert the connected or disconnected state into a connected or disconnected digital signal, and send the connected or disconnected digital signal to the signal conditioning module; Signal Conditioning Module: Receive analog signals of voltage and current from the analog acquisition module; amplify and filter the analog signals of voltage and current in turn, generate filtered and amplified voltage and current signals, and filter and amplify them Send the voltage and current signals to the upper computer module; receive the connected or disconnected digital signal from the digital acquisition module; convert the connected or disconnected digital signal into a connected or disconnected electrical signal; and send the connected or disconnected electrical signal To the host computer module; Communication module: collect the status information of the external device under test, and send the status information of the external device under test to the upper computer module and the lower computer module; Host computer module: Receive the filtered and amplified voltage and current signals from the signal conditioning module; receive the connection or disconnection electrical signal from the signal conditioning module; receive the status of the external device under test from the communication module or the lower computer module Information; store, display and monitor the filtered and amplified voltage and current signals, connect or disconnect electrical signals, and the status information of external equipment to be tested; send the control signal of the lower computer to the lower computer module to realize the control of the lower computer module control; Lower computer module: Receive the status information of the external device under test from the communication module; send the status information of the external device under test to the upper computer module; receive the lower computer control signal from the upper computer; generate the control command of the external device under test ; and send the control command of the external device under test to the external device under test through the communication module, so as to realize the control of the external device under test. 2. The aircraft ground automatic test system based on real-time serial communication according to claim 1, characterized in that: the alternating current from the external power supply system is 220V. 3. the aircraft ground automatic test system based on real-time serial communication according to claim 1, is characterized in that: when signal conditioning module receives the connected digital signal that digital acquisition module transmits, the connected digital signal is converted into 5V electric signal , and send the 5V electrical signal to the host computer module. 4. the aircraft ground automatic test system based on real-time serial communication according to claim 3, is characterized in that: when signal conditioning module receives the disconnection digital signal that digital acquisition module transmits, convert disconnection digital signal into 0V Electrical signal, and send the 0V electrical signal to the host computer module. 5. The aircraft ground automatic test system based on real-time serial communication according to claim 4, characterized in that: the status information of the external equipment to be tested includes on-board navigation data and on-board equipment status data. 6. the aircraft ground automatic test system based on real-time serial communication according to claim 1, is characterized in that: when the state information of external equipment under test is real-time sending and receiving, communication module sends the state information of external equipment under test earlier to the lower computer module; and the lower computer module sends the status information of the external device under test to the upper computer module; when the status information of the external device under test is not real-time sending and receiving, the communication module directly sends the status information of the external device under test Send to the host computer module. 7. The aircraft ground automatic test system based on real-time serial communication according to claim 1, characterized in that: the lower computer control signal includes start, stop and reset control signals to the lower computer. 8. The aircraft ground automatic test system based on real-time serial communication according to claim 1, characterized in that: said external device-under-test control instructions include navigation data control instructions and device-under-test control instructions.