CN107804479A - A kind of rudder system method of testing, device and its rudder system test equipment used - Google Patents
A kind of rudder system method of testing, device and its rudder system test equipment used Download PDFInfo
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- CN107804479A CN107804479A CN201711027563.XA CN201711027563A CN107804479A CN 107804479 A CN107804479 A CN 107804479A CN 201711027563 A CN201711027563 A CN 201711027563A CN 107804479 A CN107804479 A CN 107804479A
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/60—Testing or inspecting aircraft components or systems
Abstract
The invention discloses a kind of rudder system method of testing to include：The master control instruction that test program is sent is received, the master control instruction is the rudder system to be tested and test event generation that the test program selects according to tester；It is N bar stereotyped commands by the master control instruction extension, wherein, N is positive integer；The N bars stereotyped command is respectively sent to corresponding rudder system to be tested, so that the rudder system to be tested is tested the test event.It can be seen that, rudder system method of testing provided in an embodiment of the present invention, the test instruction of more set rudder systems is generated into a master control instruction, and more set rudder systems are realized on the basis of basic test system for the extension instructed by master control while communication and test, both test job accuracy and reliability had been can guarantee that, and can shortens the testing time of rudder system.The invention also discloses a kind of rudder system test device and its test equipment and computer-readable recording medium that use, above-mentioned technique effect can be equally realized.
Description
Technical field
The present invention relates to testing field, more specifically to a kind of rudder system method of testing, device and its rudder used
System test equipment and computer-readable recording medium.
Background technology
The test of electric rudder system steering wheel amplifier, test equipment are the supporting special test equipments of electric rudder system, are tested
The rudder system of any one in rudder system can be powered for equipment and application control signal, while the acquisition module pair of test equipment
That sampling, and send sampling quantity to test equipment this time of each signal for needing to gather of system, and according to the finger to be tested
Mark and data processing is carried out to the data measured and shown, so as to judge whether electric rudder system properties of product are up to standard.
At present, existing a variety of rudder system test systems, most of surveyed for test performance algorithm or a certain performance
Single set rudder system soft and hardware design that examination proposes, main purpose are the time for shortening single test, improve testing efficiency
And measuring accuracy.Existing rudder system test device, each test period can be only done the performance test of a set of rudder system, mainly
Rudder system for small yield is tested, and can not test more sets simultaneously, and time-consuming long, people is tested for the rudder system of production in enormous quantities
Power cost is too high.
In addition, part testing systems need tester to the composition of hardware circuit, the contact of software and hardware and signal
Chain reaction etc. has deeper understanding, it is desirable to which tester must possess high technical merit, it is difficult to fully achieves automation and surveys
Examination.
Therefore, the performance test of a variety of rudder systems how is completed simultaneously, shortens the rudder system testing time, improves testing efficiency
It is that those skilled in the art need to solve the problems, such as.
The content of the invention
It is an object of the invention to provide a kind of rudder system method of testing, device and its test equipment used and computer
Readable storage medium storing program for executing, while the performance test of a variety of rudder systems is completed, shorten the rudder system testing time, improve testing efficiency.
To achieve the above object, the embodiments of the invention provide a kind of rudder system method of testing, including：
The master control instruction that test program is sent is received, the master control instruction is the test program according to tester
Rudder system to be tested and the test event generation of selection；
It is N bar stereotyped commands by the master control instruction extension, wherein, N is positive integer；
The N bars stereotyped command is respectively sent to corresponding rudder system to be tested, so as to the rudder system pair to be tested
The test event is tested.
Wherein, after the N bars stereotyped command being respectively sent into corresponding rudder system, in addition to：
The test feedback command that the rudder system to be tested is sent is received, is comprised at least in the test feedback command described
The positional information of rudder system to be tested；
All test feedback commands are integrated into total feedback command；
Total feedback command is sent to the test program, so that test program parsing total feedback refers to
Order.
Wherein, after the test program parsing total feedback command, in addition to：
The test program preserves parsing and obtains the positional information of each rudder system to be tested, and the position is believed
Breath is shown to human-computer interaction interface.
Wherein, master control instruction is including at least the position control signal of all rudder systems to be tested and standby
Position, each corresponding rudder system of the spare bit, whether rudder system corresponding to the state representation of each is to be tested
Rudder system.
Wherein, it is that N bar stereotyped commands include by the master control instruction extension：
The position control signal is split as N bar position control signals by the numbering of rudder system, and corresponded to after splitting
Position control signal of the position control signal as nth bar stereotyped command；
Spare bit in the N bars stereotyped command is arranged to preset value, wherein n is the positive integer no more than N.
Wherein, the test feedback command is integrated into total feedback command includes：
The positional information of all test feedback commands is merged into the positional information of total feedback command；
According to the spare bit of the state of all rudder systems generation total test feedback command, the spare bit each
A corresponding rudder system, whether rudder system corresponding to the state representation of each is rudder system to be tested..
To achieve the above object, the embodiments of the invention provide a kind of rudder system test device, including：
First receiving module, for receiving the master control instruction of test program transmission, the master control instruction is the survey
What the rudder system to be tested and test event that examination program selects according to tester generated；
Expansion module, for being N bar stereotyped commands by the master control instruction extension, wherein, N is positive integer；
First sending module, for the N bars stereotyped command to be respectively sent into corresponding rudder system, so as to the rudder system
System starts to test.
Wherein, in addition to：
Second receiving module, the test feedback command sent for receiving the rudder system are described to test in feedback command
Including at least the positional information of the rudder system；
Module is integrated, for all test feedback commands to be integrated into total feedback command；
Second sending module, for total feedback command to be sent to the test program, so as to the test program
Parse total feedback command.
To achieve the above object, the embodiments of the invention provide a kind of test equipment, including：
Memory, for storing rudder system test program；
Processor, the rudder system as described in any one of claim 1 to 6 is realized during for performing the rudder system test program
The step of method of testing.
To achieve the above object, the embodiments of the invention provide a kind of computer-readable recording medium, the computer can
Read to be stored with rudder system test program in storage medium, realize when the rudder system test program is executed by processor and appoint as described above
One rudder system method of testing.
By above scheme, a kind of rudder system method of testing provided in an embodiment of the present invention includes：Receive test journey
The master control instruction that sequence is sent, the rudder system to be tested that the master control instruction selects for the test program according to tester
With test event generation；It is N bar stereotyped commands by the master control instruction extension, wherein, N is positive integer；By the N bars mark
Quasi instruction is respectively sent to corresponding rudder system to be tested, so that the rudder system to be tested is surveyed to the test event
Examination.
As can be seen here, rudder system method of testing provided in an embodiment of the present invention, the test of more set rudder systems is instructed into generation
One master control instruction, and the extension instructed by master control realizes more set rudder systems simultaneously on the basis of basic test system
Communication and test, both can guarantee that test job accuracy and reliability, and can greatly shortens the testing time of rudder system.The present invention
A kind of rudder system test device and its test equipment and computer-readable recording medium that use are also disclosed, can equally be realized
State technique effect.
Brief description of the drawings
In order to illustrate more clearly about the embodiment of the present invention or technical scheme of the prior art, below will be to embodiment or existing
There is the required accompanying drawing used in technology description to be briefly described, it should be apparent that, drawings in the following description are only this
Some embodiments of invention, for those of ordinary skill in the art, on the premise of not paying creative work, can be with
Other accompanying drawings are obtained according to these accompanying drawings.
Fig. 1 is a kind of flow chart of rudder system method of testing disclosed in the embodiment of the present invention；
Fig. 2 is the wiring schematic diagram that a kind of rudder system method of testing disclosed in the embodiment of the present invention instructs modular converter；
Fig. 3 is the flow chart of another rudder system method of testing disclosed in the embodiment of the present invention；
Fig. 4 is the flow chart of another rudder system method of testing disclosed in the embodiment of the present invention；
Fig. 5 is the schematic diagram of another rudder system method of testing instruction extension disclosed in the embodiment of the present invention；
Fig. 6 is the schematic diagram that another rudder system method of testing instruction disclosed in the embodiment of the present invention is integrated；
Fig. 7 is a kind of structure chart of rudder system test device disclosed in the embodiment of the present invention；
Fig. 8 is a kind of structure chart of test equipment disclosed in the embodiment of the present invention.
Embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out clear, complete
Site preparation describes, it is clear that described embodiment is only part of the embodiment of the present invention, rather than whole embodiments.It is based on
Embodiment in the present invention, those of ordinary skill in the art are obtained every other under the premise of creative work is not made
Embodiment, belong to the scope of protection of the invention.
The embodiment of the invention discloses a kind of rudder system method of testing, while the performance test of a variety of rudder systems is completed, contracted
The short rudder system testing time, improve testing efficiency.
Referring to Fig. 1 and Fig. 2, Fig. 1 is that a kind of flow chart of rudder system method of testing, Fig. 2 disclosed in the embodiment of the present invention are
A kind of wiring schematic diagram of rudder system method of testing instruction modular converter disclosed in the embodiment of the present invention, as shown in figure 1, including：
S101：The master control instruction that test program is sent is received, the master control instruction is the test program according to survey
What the rudder system to be tested and test event of examination personnel selection generated；
In specific implementation, a personal-machine interactive interface can be designed for test program, interface includes rudder system model, surveyed
Test ring border explanation, tested rudder system select, test event selects, communicate serial ports configuration, start testing button module and test to report
Table display box etc., the module subregion of human-computer interaction interface is clear, is easily understood.
On human-computer interaction interface, tester can arbitrarily select need test rudder system numbering, steering wheel numbering with
And test event, click on test program generation after starting to test covers rudder system more master control instruction one.
S102：It is N bar stereotyped commands by the master control instruction extension, wherein, N is positive integer；
In specific implementation, master control is instructed and exported by test program, as shown in Fig. 2 the signal of output is differential signal,
By two pin outputs of TX422+, TX422-, then differential signal is converted to single-end output signal by communication chip, is passed through
TX422 pins are sent to FPGA main control chips, after FPGA main control chips receive master control instruction, by the master control instruction extension
For N bar stereotyped commands, N is corresponding with the rudder system to be tested that tester selects, i.e., tester have selected several rudders to be tested
System, master control instruction can expand to several stereotyped commands.
S103：The N bars stereotyped command is respectively sent to corresponding rudder system to be tested, so as to the rudder system to be tested
System is tested the test event.
In specific implementation, by control instruction pass through corresponding to pin be sent to communication chip, by single ended signal turn
After being changed to differential signal, corresponding tested rudder system is sent to by corresponding pin.
Rudder system method of testing provided in an embodiment of the present invention, by test instruction one master control of generation of more set rudder systems
Instruction, and the extension instructed by master control realizes more set rudder systems on the basis of basic test system while communicates and survey
Examination, both can guarantee that test job accuracy and reliability, and can greatly shortens the testing time of rudder system.
The embodiment of the invention discloses a kind of rudder system method of testing, and relative to a upper embodiment, the present embodiment is to technology
Scheme has made further instruction and optimization.Specifically：
Referring to Fig. 3, Fig. 3 is the flow chart of another rudder system method of testing provided in an embodiment of the present invention, such as Fig. 3 institutes
Show, including：
S301：The master control instruction that test program is sent is received, the master control instruction is the test program according to survey
What the rudder system to be tested and test event of examination personnel selection generated；
S302：It is N bar stereotyped commands by the master control instruction extension, wherein, N is positive integer；
S303：The N bars stereotyped command is respectively sent to corresponding rudder system to be tested, so as to the rudder system to be tested
System is tested the test event.
S304：The test feedback command that the rudder system to be tested is sent is received, is at least wrapped in the test feedback command
Positional information containing the rudder system to be tested；
It is understood that the positional information of the rudder system to be tested included in test feedback command, i.e., rudder system to be tested
The test result of system.Certainly, test feedback command can also include other guide, be consistent with the form of stereotyped command,
This is not especially limited.
S305：All test feedback commands are integrated into total feedback command；
S306：Total feedback command is sent to the test program, so that test program parsing is described total anti-
Feedback instruction.
In specific implementation, the merging process of feedback command is tested with the expansion process of master control instruction on the contrary, communicating
Chip is received the test feedback command of rudder system to be measured by corresponding pin, after differential signal is converted into single ended signal,
FPGA main control chips are sent to by corresponding pin, after FPGA main control chips receive test feedback command, by all surveys
Examination feedback command is integrated into total feedback command, and communication chip is sent to by RX422 pins, and by RX422+, RX422- two
Pin is exported to test program.
On the basis of above-described embodiment, preferably, the master control instruction comprises at least all described
The position control signal and spare bit of rudder system to be tested, each corresponding rudder system of the spare bit, each
Whether rudder system corresponding to state representation is rudder system to be tested.
In specific implementation, master control instruction frame format comprises at least the position control letter of all rudder systems to be tested
Number and spare bit, naturally it is also possible to including frame head, ID and check bit.The meaning of frame head, ID and check bit in control instruction with
Frame head, ID are identical with the meaning of check bit in standard control instruction；Position control signal is made up of one or more groups of data, is often covered
The corresponding one group of data of rudder system, i.e. tester have selected several rudder systems to be tested, and position control signal is just by several groups of data
Composition, the form and expression meaning of every group of data are identical with the form of data bit and meaning in standard control instruction；Spare bit table
Show and selected rudder system number information, it is defined as follows：Whether rudder system selects to use binary representation, and " 1 " represents to have selected, " 0 " table
Show it is unselected, by the binary value of all rudder system selection results composition by hexadecimal representation, if two bytes and more than, first
Low byte is passed, then passes high byte.
For example, test more set rudder system test systems of 10 sets of rudder systems simultaneously for most multipotency, and in certain test, choosing
All steering wheels of rudder system numbering XX01 and XX06 and this two sets of rudder systems are selected, arbitrarily select a test event to start to test
Afterwards, the control instruction of test program generation is：Frame head+ID+XX01 rudder system control information+XX06 rudder systems control information+
2100+ verify and.
It is stereotyped command, total anti-it is understood that all instructions involved by the embodiment of the present invention, i.e. master control instruct
Feedback instruction and test feedback command can include the above, i.e. frame head, ID, the position control signal of rudder system, spare bit
With verification and, but the data bits of each section can be adjusted according to actual conditions.
On the basis of above-described embodiment, preferably, the test program parses total feedback command
Afterwards, in addition to：
The test program preserves parsing and obtains the positional information of each rudder system to be tested, and the position is believed
Breath is shown to human-computer interaction interface.
After test program receives feedback command, first determine whether verification and then parse spare bit, while split out tested rudder
The feedback position signal of system, position signalling is corresponding with tested rudder system numbering, and real-time display simultaneously preserves tested rudder system
Positional information, test are completed to post-process all positional informations, analyze the performance of tested rudder system and judge whether test performance is full
Foot requires that generation test report shows the test process that a test event is completed to human-computer interaction interface.
The embodiment of the invention discloses a kind of rudder system method of testing, and relative to a upper embodiment, the present embodiment is to technology
Scheme has made further instruction and optimization.Specifically：
Referring to Fig. 4, Fig. 5 and Fig. 6, Fig. 4 is the flow chart of another rudder system method of testing provided in an embodiment of the present invention,
Fig. 5 is the schematic diagram of another rudder system method of testing instruction extension disclosed in the embodiment of the present invention, and Fig. 6 is the embodiment of the present invention
The schematic diagram that disclosed another rudder system method of testing instruction is integrated, as shown in figure 4, including：
S401：The master control instruction that test program is sent is received, the master control instruction is the test program according to survey
What the rudder system to be tested and test event of examination personnel selection generated；
S421：The position control signal is split as N bar position control signals by the numbering of rudder system, and by after fractionation
Position control signal of the corresponding position control signal as nth bar stereotyped command, wherein, N is positive integer, and wherein n is little
In N positive integer；
S422：Spare bit in N bar stereotyped commands is arranged to preset value；
It should be noted that each stereotyped command can include the position control signal, standby of frame head, ID, rudder system
Position and verification and.Wherein, the frame head of stereotyped command, ID and verification and consistent with master control instruction.The check value of stereotyped command leads to
Often in the case of be fixed, for example, verification that can be by stereotyped command and each be all set to 0.The position control of stereotyped command
Signal is that the position control signal of master control instruction splits what is obtained.
In specific implementation, master control is instructed and exported by test program, as shown in Fig. 2 the signal of output is differential signal,
By two pin outputs of TX422+, TX422-, then differential signal is converted to single-end output signal by communication chip, is passed through
TX422 pins are sent to FPGA main control chips, after FPGA main control chips receive master control instruction, split frame head, ID and control
The frame structure informations such as information, it is last as shown in figure 5, being required according to the communication frame format of rudder system model definition to be tested, combination
Generate a plurality of complete standard control instruction, every standard control instruction form is identical, and with rudder system model definition to be tested
Communication frame format it is consistent, while parse spare bit to determine that rudder system to be tested is numbered.
S403：The N bars stereotyped command is respectively sent to corresponding rudder system to be tested, so as to the rudder system to be tested
System is tested the test event.
In specific implementation, control instruction is sent to communication chip by pin 1TX422 and 6TX422, will be single-ended defeated
Enter after signal is converted to differential signal, by pin 1TX422+, 1TX422- and 6TX422+, 6TX422- be sent to corresponding to it is to be measured
Try rudder system.
S404：The test feedback command that the rudder system to be tested is sent is received, is at least wrapped in the test feedback command
Positional information containing the rudder system to be tested；
S451：The positional information of all test feedback commands is merged into the positional information of total feedback command；
S452：The spare bit of total test feedback command is generated according to the state of all rudder systems, the spare bit
Each corresponding rudder system, whether rudder system corresponding to the state representation of each is rudder system to be tested；
It is understood that the process for integrating total feedback command is opposite with the process for splitting master control instruction.In above-mentioned example
In son, numbering be XX01 and XX06 rudder system receive control instruction after start to act, and feed back current position state, feedback
Differential signal is sent to communication chip by pin 1RX422+, 1RX422- and 6RX422+, 6RX422- respectively, and communication chip will
Differential input signal is converted to single-end output signal, is sent to fpga chip by pin 1RX422 and 6RX422, fpga chip is such as
Shown in Fig. 6, first determine whether every control instruction verification and, then judge tested rudder system by receiving the pin number of signal
Numbering, and then the value of spare bit is calculated, while the position signalling of feedback command is split out, finally by frame head, ID, feedback bit confidence
Number and spare bit integrate, calculate verification and, generate a complete total feedback command.
S406：Total feedback command is sent to the test program, so that test program parsing is described total anti-
Feedback instruction.
A kind of rudder system test device provided in an embodiment of the present invention is introduced below, a kind of rudder system described below
Guided Missiles Service Test Set can be with cross-referenced with a kind of above-described rudder system method of testing.
Referring to Fig. 7, a kind of structure chart of rudder system test device provided in an embodiment of the present invention, as shown in fig. 7, comprises：
First receiving module 701, for receiving the master control instruction of test program transmission, the master control instruction is described
Rudder system to be tested and the test event generation that test program selects according to tester；
Expansion module 702, for being N bar stereotyped commands by the master control instruction extension, wherein, N is positive integer；
First sending module 703, for the N bars stereotyped command to be respectively sent into corresponding rudder system, so as to described
Rudder system starts to test.
Rudder system test device provided in an embodiment of the present invention, by test instruction one master control of generation of more set rudder systems
Instruction, and the extension instructed by master control realizes more set rudder systems on the basis of basic test system while communicates and survey
Examination, both can guarantee that test job accuracy and reliability, and can greatly shortens the testing time of rudder system.
On the basis of above-described embodiment, preferably, in addition to：
Second receiving module, the test feedback command sent for receiving the rudder system are described to test in feedback command
Including at least the positional information of the rudder system；
Module is integrated, for all test feedback commands to be integrated into total feedback command；
Second sending module, for total feedback command to be sent to the test program, so as to the test program
Parse total feedback command.
On the basis of above-described embodiment, preferably, in addition to：
Display module, the positional information of each rudder system to be tested is obtained for preserving parsing, and by the position
Presentation of information is to human-computer interaction interface.
Present invention also provides a kind of test equipment, referring to Fig. 8, a kind of knot of test equipment provided in an embodiment of the present invention
Composition, as shown in figure 8, including：
Memory 801, for storing rudder system test program；
Processor 802, the step of above-described embodiment provides can be realized during for performing the rudder system test program.
Certain test equipment can also include the component such as various network interfaces, power supply.
Present invention also provides a kind of computer-readable recording medium, is stored thereon with rudder system test program, the rudder
System testing program can realize the step of above-described embodiment provides when being executed by processor.The storage medium can include：U
Disk, mobile hard disk, read-only storage (Read-Only Memory, ROM), random access memory (Random Access
Memory, RAM), magnetic disc or CD etc. are various can be with the medium of store program codes.
Each embodiment is described by the way of progressive in this specification, what each embodiment stressed be and other
The difference of embodiment, between each embodiment identical similar portion mutually referring to.
The foregoing description of the disclosed embodiments, professional and technical personnel in the field are enable to realize or using the present invention.
A variety of modifications to these embodiments will be apparent for those skilled in the art, as defined herein
General Principle can be realized in other embodiments without departing from the spirit or scope of the present invention.Therefore, it is of the invention
The embodiments shown herein is not intended to be limited to, and is to fit to and principles disclosed herein and features of novelty phase one
The most wide scope caused.
Claims (10)
- A kind of 1. rudder system method of testing, it is characterised in that including：The master control instruction that test program is sent is received, the master control instruction selects for the test program according to tester Rudder system to be tested and test event generation；It is N bar stereotyped commands by the master control instruction extension, wherein, N is positive integer；The N bars stereotyped command is respectively sent to corresponding rudder system to be tested, so that the rudder system to be tested is to described Test event is tested.
- 2. rudder system method of testing according to claim 1, it is characterised in that send the N bars stereotyped command respectively To corresponding rudder system, in addition to：The test feedback command that the rudder system to be tested is sent is received, is comprised at least in the test feedback command described to be measured Try the positional information of rudder system；All test feedback commands are integrated into total feedback command；Total feedback command is sent to the test program, so that the test program parses total feedback command.
- 3. rudder system method of testing according to claim 2, it is characterised in that test program parsing total feedback After instruction, in addition to：The test program preserves parsing and obtains the positional information of each rudder system to be tested, and the positional information is shown Show to human-computer interaction interface.
- 4. according to the rudder system method of testing described in claim any one of 1-3, it is characterised in that the master control instruction is at least Include the position control signal and spare bit of all rudder systems to be tested, each corresponding rudder system of the spare bit System, whether rudder system corresponding to the state representation of each is rudder system to be tested.
- 5. rudder system method of testing according to claim 4, it is characterised in that by the master control instruction extension be N bars Stereotyped command includes：The position control signal is split as N bar position control signals by the numbering of rudder system, and corresponding position after splitting Put position control signal of the control signal as nth bar stereotyped command；Spare bit in the N bars stereotyped command is arranged to preset value, wherein n is the positive integer no more than N.
- 6. rudder system method of testing according to claim 5, it is characterised in that be integrated into the test feedback command always Feedback command includes：The positional information of all test feedback commands is merged into the positional information of total feedback command；It is corresponding according to the spare bit of the state of all rudder systems generation total test feedback command, each of the spare bit Whether one rudder system, rudder system corresponding to the state representation of each are rudder system to be tested.
- A kind of 7. rudder system test device, it is characterised in that including：First receiving module, for receiving the master control instruction of test program transmission, the master control instruction is the test journey Rudder system to be tested and the test event generation that sequence selects according to tester；Expansion module, for being N bar stereotyped commands by the master control instruction extension, wherein, N is positive integer；First sending module, for the N bars stereotyped command to be respectively sent into corresponding rudder system, so that the rudder system is opened Begin to test.
- 8. rudder system test device according to claim 7, it is characterised in that also include：Second receiving module, the test feedback command sent for receiving the rudder system are described to test in feedback command at least Include the positional information of the rudder system；Module is integrated, for all test feedback commands to be integrated into total feedback command；Second sending module, for total feedback command to be sent to the test program, so that the test program parses Total feedback command.
- A kind of 9. rudder system test equipment, it is characterised in that including：Memory, for storing rudder system test program；Processor, the rudder system test as described in any one of claim 1 to 6 is realized during for performing the rudder system test program The step of method.
- 10. a kind of computer-readable recording medium, it is characterised in that be stored with rudder system on the computer-readable recording medium Test program, realize that rudder system is surveyed as described in any one of claim 1 to 6 when the rudder system test program is executed by processor Method for testing.
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111999707A (en) * | 2020-08-19 | 2020-11-27 | 无锡威孚高科技集团股份有限公司 | Automatic testing method, device and system for millimeter wave radar |
| CN116296345A (en) * | 2023-05-11 | 2023-06-23 | 西安晟昕科技股份有限公司 | Steering engine performance test method |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5978902A (en) * | 1997-04-08 | 1999-11-02 | Advanced Micro Devices, Inc. | Debug interface including operating system access of a serial/parallel debug port |
| CN1540923A (en) * | 2003-10-29 | 2004-10-27 | 中兴通讯股份有限公司 | Online remote method for upgrating time slot convergence devices |
| CN103558838A (en) * | 2013-11-01 | 2014-02-05 | 北京航空航天大学 | Solid-liquid power air vehicle ground test and launch control system of 422 bus |
| CN104780140A (en) * | 2014-01-12 | 2015-07-15 | 盛吉高科（北京）科技有限公司 | Configurable communication protocol identifying and parsing system |
| CN204832366U (en) * | 2015-03-11 | 2015-12-02 | 张家港智电柔性输配电技术研究所有限公司 | Direct screening formula high pressure chain SVG chain link testing arrangement |
| CN105783612A (en) * | 2016-03-28 | 2016-07-20 | 北京航天控制仪器研究所 | General miniaturization digital electric steering engine controller and control method thereof |
| CN106645940A (en) * | 2016-11-30 | 2017-05-10 | 中国航天空气动力技术研究院 | Digital rudder system frequency response characteristic testing device and method |
| CN106844195A (en) * | 2016-12-22 | 2017-06-13 | 福建瑞之付微电子有限公司 | A kind of method of testing based on the test of unified instruction collection |
-
2017
- 2017-10-27 CN CN201711027563.XA patent/CN107804479B/en active Active
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5978902A (en) * | 1997-04-08 | 1999-11-02 | Advanced Micro Devices, Inc. | Debug interface including operating system access of a serial/parallel debug port |
| CN1540923A (en) * | 2003-10-29 | 2004-10-27 | 中兴通讯股份有限公司 | Online remote method for upgrating time slot convergence devices |
| CN103558838A (en) * | 2013-11-01 | 2014-02-05 | 北京航空航天大学 | Solid-liquid power air vehicle ground test and launch control system of 422 bus |
| CN104780140A (en) * | 2014-01-12 | 2015-07-15 | 盛吉高科（北京）科技有限公司 | Configurable communication protocol identifying and parsing system |
| CN204832366U (en) * | 2015-03-11 | 2015-12-02 | 张家港智电柔性输配电技术研究所有限公司 | Direct screening formula high pressure chain SVG chain link testing arrangement |
| CN105783612A (en) * | 2016-03-28 | 2016-07-20 | 北京航天控制仪器研究所 | General miniaturization digital electric steering engine controller and control method thereof |
| CN106645940A (en) * | 2016-11-30 | 2017-05-10 | 中国航天空气动力技术研究院 | Digital rudder system frequency response characteristic testing device and method |
| CN106844195A (en) * | 2016-12-22 | 2017-06-13 | 福建瑞之付微电子有限公司 | A kind of method of testing based on the test of unified instruction collection |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111999707A (en) * | 2020-08-19 | 2020-11-27 | 无锡威孚高科技集团股份有限公司 | Automatic testing method, device and system for millimeter wave radar |
| CN116296345A (en) * | 2023-05-11 | 2023-06-23 | 西安晟昕科技股份有限公司 | Steering engine performance test method |
| CN116296345B (en) * | 2023-05-11 | 2023-08-15 | 西安晟昕科技股份有限公司 | Steering engine performance test method |
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