CN110955592A - Method and device for testing flight training simulator software - Google Patents
Method and device for testing flight training simulator software Download PDFInfo
- Publication number
- CN110955592A CN110955592A CN201911001001.7A CN201911001001A CN110955592A CN 110955592 A CN110955592 A CN 110955592A CN 201911001001 A CN201911001001 A CN 201911001001A CN 110955592 A CN110955592 A CN 110955592A
- Authority
- CN
- China
- Prior art keywords
- software
- test
- flight
- training simulator
- flight training
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Images
Classifications
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F11/00—Error detection; Error correction; Monitoring
- G06F11/36—Preventing errors by testing or debugging software
- G06F11/3604—Software analysis for verifying properties of programs
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F11/00—Error detection; Error correction; Monitoring
- G06F11/36—Preventing errors by testing or debugging software
- G06F11/3664—Environments for testing or debugging software
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F11/00—Error detection; Error correction; Monitoring
- G06F11/36—Preventing errors by testing or debugging software
- G06F11/3668—Software testing
- G06F11/3672—Test management
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F11/00—Error detection; Error correction; Monitoring
- G06F11/36—Preventing errors by testing or debugging software
- G06F11/3668—Software testing
- G06F11/3672—Test management
- G06F11/3684—Test management for test design, e.g. generating new test cases
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F11/00—Error detection; Error correction; Monitoring
- G06F11/36—Preventing errors by testing or debugging software
- G06F11/3668—Software testing
- G06F11/3672—Test management
- G06F11/3688—Test management for test execution, e.g. scheduling of test suites
Landscapes
- Engineering & Computer Science (AREA)
- Theoretical Computer Science (AREA)
- Computer Hardware Design (AREA)
- Quality & Reliability (AREA)
- Physics & Mathematics (AREA)
- General Engineering & Computer Science (AREA)
- General Physics & Mathematics (AREA)
- Software Systems (AREA)
- Debugging And Monitoring (AREA)
Abstract
The invention relates to a test method and a device for flight training simulator software, which are used for analyzing two aspects of software characteristics and software scenes according to documents such as a flight training simulator software task book, a requirement specification description and the like submitted by a development unit to obtain software test requirements; on the basis of the analyzed software test requirements, establishing a test environment and generating a software test case; executing the test case on the submitted tested software, acquiring the test result, and taking corresponding measures according to different judgment results; and finally, summarizing the test process and the test result of the flight training simulator software, and giving out the evaluation conclusion of the software and the software quality evaluation, wherein the software quality evaluation comprises document quality evaluation and program quality evaluation. The invention tests all links of the flight training simulator software in all directions, realizes the reliability and safety of the software, and fills the blank that no relevant mature test scheme specially aiming at the flight training simulator software exists at present.
Description
Technical Field
The invention relates to a method and a device for testing flight training simulator software, and belongs to the technical field of computer software.
Background
A flight training simulator is a system for reproducing or simulating the flight experience of an airplane as truly as possible, and can reproduce various environments such as air and ground and perform operation control.
With the development of computer systems and software technologies, the performance of flight training simulators is continuously improved, and the flight training simulators become indispensable important training equipment for guaranteeing flight safety, greatly improving the skills of flight personnel and flight crew, shortening the training period of the flight personnel, reducing the training cost and improving the training efficiency. The flight simulation system is utilized to systematically train pilots, and the flight simulation system has the outstanding advantages of energy conservation, economy, safety, no limitation of field and weather conditions, short training period, high training efficiency and the like. The training of various complex flight environments, flight failure states, military missile evasion technologies and the like can be carried out on the flight training simulator, and the training by utilizing the simulator is an indispensable link for training general aviation pilots and special operating personnel and is also an important source for transporting aviation and military aviation professional talents. Therefore, the test of the flight training simulator is also important.
However, currently, the software of the flight training simulator is specially used for less related test methods, and more mature test models are fewer.
Disclosure of Invention
The invention aims to provide a method and a device for testing flight training simulator software, which aim to overcome the defects of the prior art.
The invention provides a test method of flight training simulator software, which comprises the following steps:
analyzing from two aspects of software characteristics and software scenes according to submitted software task books and requirement specification of the flight training simulator to obtain software testing requirements;
on the basis of the analyzed software test requirements, establishing a test environment and generating a software test case;
executing the test case on the submitted tested software, acquiring the test result, and taking corresponding measures according to different judgment results;
and summarizing the test process and the test result of the flight training simulator software, and giving an evaluation conclusion of the software and software quality evaluation, wherein the software quality evaluation comprises document quality evaluation and program quality evaluation.
Further, the analyzing the characteristics of the software comprises:
the basic software function is that the functional composition and the working process of the software are known according to a software task book and a requirement specification document submitted by a developer;
a software crosslinking environment, including a software environment and a hardware environment;
user type and mode of use;
and the software running state comprises stand-alone running and networking running.
Further, the analyzing of the scene of the software includes: flight environment, flight failure state, launching process of various weapons, flight evasion to different missiles, tactical countermeasure between airplanes, and tactical maneuvering.
Further, the test case comprises input data, test conditions, test procedures and expected results, and the test procedures in the test case comprise preparation, initialization, execution steps and end conditions of the test case.
Further, the executing the test case on the submitted tested software, while obtaining the test result, taking corresponding measures according to different judgment results, specifically: and checking the normal and abnormal termination conditions of the test process, and determining whether to stop the test or to modify or supplement the test case set according to the check result for the test cases which do not reach the test termination condition, and further testing.
A test apparatus for flight training simulator software, comprising:
the software testing requirement analysis module is used for analyzing the characteristics of software and a software scene according to the submitted flight training simulator software task book and requirement specification to obtain a software testing requirement;
the software test design and realization module is used for establishing a test environment and generating a software test case on the basis of the analyzed software test requirements;
the software test execution module executes the test case for the submitted tested software, acquires the test result and takes corresponding measures according to different judgment results;
and the software test result module is used for summarizing the test process and the test result of the flight training simulator software and giving an evaluation conclusion of the software and software quality evaluation, wherein the software quality evaluation comprises document quality evaluation and program quality evaluation.
Further, the analysis of the software testing requirement analysis module on the characteristics of the software comprises:
the basic software function is that the functional composition and the working process of the software are known according to a software task book and a requirement specification document submitted by a developer;
a software crosslinking environment, including a software environment and a hardware environment;
user type and mode of use;
and the software running state comprises stand-alone running and networking running.
Further, the analysis of the software testing requirement analysis module on the software scene includes: flight environment, flight failure state, launching process of various weapons, flight evasion to different missiles, tactical countermeasure between airplanes, and tactical maneuvering.
Further, the test case generated by the software test design and implementation module comprises input data, test conditions, test procedures and expected results, and the test procedures in the test case comprise preparation, initialization, execution steps and end conditions of the test case.
Further, the software test execution module executes the test case on the submitted software to be tested, acquires the test result, and takes corresponding measures according to different judgment results, specifically: and checking the normal and abnormal termination conditions of the test process, and determining whether to stop the test or to modify or supplement the test case set according to the check result for the test cases which do not reach the test termination condition, and further testing.
The invention has the beneficial effects that:
according to documents such as a flight training simulator software task book and a requirement specification submitted by a development unit, the software testing requirement is obtained by analyzing two aspects of software characteristics and a software scene; on the basis of the analyzed software test requirements, establishing a test environment and generating a software test case; executing the test case on the submitted tested software, acquiring the test result, and taking corresponding measures according to different judgment results; and finally, summarizing the test process and the test result of the flight training simulator software, and giving out the evaluation conclusion of the software and the software quality evaluation, wherein the software quality evaluation comprises document quality evaluation and program quality evaluation. All links of the flight training simulator software are tested in an all-around manner by utilizing all detection models, so that the reliability and the safety of the software are realized, and the blank that no related mature test scheme specially aiming at the flight training simulator software exists at present is filled.
Drawings
FIG. 1 is a flow chart of an embodiment of the method of the present invention.
FIG. 2 is a schematic block diagram of an apparatus according to an embodiment of the present invention.
Detailed Description
The invention will now be described in further detail with reference to the accompanying drawings:
as shown in fig. 1, an embodiment of the present invention provides a method for testing flight training simulator software, including the steps of:
s1, analyzing from two aspects of software characteristics and software scenes according to submitted documents such as flight training simulator software task books, requirement specification descriptions and the like to obtain software testing requirements;
s2, establishing a test environment and generating a software test case on the basis of the analyzed software test requirements;
s3, executing the test case for the submitted tested software, acquiring the test result, and taking corresponding measures according to different judgment results;
and S4, summarizing the test process and the test result of the flight training simulator software, and giving out the evaluation conclusion of the software and the software quality evaluation, wherein the software quality evaluation comprises document quality evaluation and program quality evaluation.
In step S1, the analysis of the software features includes the following aspects:
1) basic functions of software. According to documents such as a software task book, a requirement specification and the like submitted by a developer, the functional composition and the working process of the software are comprehensively and deeply known.
2) Software cross-linking environment. Including software environments and hardware environments. The flight training simulator generally comprises an instructor console, a cockpit, interface equipment, a central console, a vision system and the like, and corresponding software is arranged in each equipment. For example, the vision software in the vision system can provide the scene simulation of the student, the student feels the motions of diving, pitching and circling just like sitting in the airplane during the operation, and can also see various scenes (cloud, fog, river and building) on and off the airplane, and various flight environments can be set so as to comprehensively exercise the technology and learn and master various operations with high difficulty and danger.
3) User type and mode of use. For flight training simulators, users are often pilots, commanders and coaches; the use mode can be changed according to factors such as user type, use purpose and the like, for example, the flight training device can be divided into a single task flight training device and a full task flight simulator according to a training task. The single-task flight simulation trainer is a simulator developed for training a certain flight stage or a certain operation task, and the full-task flight training simulator is a training simulator taking the whole flight process and all flight tasks as task targets.
4) Software running state. Such as stand-alone operation, networked operation.
In step S1, the analysis of the software scenario includes the following:
1) and (4) a flying environment. The flight training simulator can simulate the environment encountered during flight, such as different meteorology (blue sky, rain, snow, fog, wind), terrain (plain, mountain, basin), day and night, etc.
2) A flight failure condition. The flight personnel may need to simulate certain special flight conditions during the training process, such as fire control system faults, flight control faults, single shot failures and the like.
3) The process of launching various weapons. If the simulation of launching, guidance, flight trajectory and tactical training pod airborne of airborne air-to-air missile weapons is completed, training damage results and the like are carried out in the training task implementation stage.
4) Evasion to the flight of different missiles. It may also be desirable for a fighter pilot to train how to evade the missile using different flight techniques, such as launching jammers, infrared decoys, electronic warfare pods, etc.
5) Tactical countermeasure between aircraft. Such as a one-to-one simple air, many-to-many competition between teams, etc.
6) Tactical maneuvers. The maneuverability is one of main indexes for evaluating the performance of military aircrafts, particularly fighters, and is divided into maneuvering flight in a vertical plane, a horizontal plane and a three-dimensional space from the view of the movement track of the aircrafts. Maneuvering flight in the vertical plane mainly comprises plane flight acceleration and deceleration, dive, jump, somersault and the like; a typical action for maneuvering in the horizontal plane is horizontal hover; the maneuvering flight in three-dimensional space is commonly provided with oblique muscle fight, tactical turning, rolling, fighting half rolling and the like.
In step S2, on the basis of the analyzed software test requirements, establishing a test environment and generating a software test case, specifically:
1) and establishing a test environment. Normally, the test environment should be as identical as possible to the real operating environment. If the real test environment is limited, the simulation test environment can also be used for testing, but the simulation test environment must meet the interface requirements set forth in the task book or requirements.
2) And generating a test case. Basically after the test requirements are analyzed, test design is carried out according to the evaluation range, the evaluation items and the test input characteristics of the tested software, and test cases are compiled, wherein the test cases comprise the following steps:
① test input and test environment including hardware and software test environment;
② testing input mode and classification, wherein the input mode includes direct operation, test panel, data file, etc., and the classification includes continuity/discreteness, direct input/related test input/failure test input, etc.;
③ testing relationships between inputs, including order, concurrency, constraints, etc.;
the test case comprises input data, test conditions, test procedures and expected results, and the test procedures in the test case comprise preparation, initialization, execution steps and end conditions of the test case. The test case set can ensure that the requirements of the specified level test on the test quality are met.
Acquiring and verifying test data in the test process; determining the execution sequence of the test cases according to the constraint conditions such as test resources, risks and the like; acquiring test resources, and developing test software if necessary; and establishing and calibrating a test environment, and performing pre-operation on a test case before test execution.
And the test instruction is reviewed, the correctness, the effectiveness and the coverage integrity of the test case are mainly reviewed, and a test organization, a test environment and related equipment tools are reviewed to be complete and meet the requirements.
In step S3, the tester executes the test case on the software to be tested submitted in the development unit, and takes corresponding measures according to different determination results while obtaining the test result, if the result is consistent with the expected result or the error is in a certain unit, the case passes, otherwise, the case does not pass; and checking the normal and abnormal termination conditions of the test process, and determining whether to stop the test or to modify or supplement the test case set for the test case which does not reach the test termination condition according to the check result, and further testing.
The test procedures, results, and errors and faults discovered should be faithfully recorded during execution.
As shown in fig. 2, an embodiment of the present invention further provides a testing apparatus for flight training simulator software, including:
the software testing requirement analysis module is used for analyzing the characteristics of software and a software scene according to the submitted flight training simulator software task book and requirement specification to obtain a software testing requirement;
the software test design and realization module is used for establishing a test environment and generating a software test case on the basis of the analyzed software test requirements;
the software test execution module executes the test case for the submitted tested software, acquires the test result and takes corresponding measures according to different judgment results;
and the software test result module is used for summarizing the test process and the test result of the flight training simulator software and giving an evaluation conclusion of the software and software quality evaluation, wherein the software quality evaluation comprises document quality evaluation and program quality evaluation.
The working flows and principles of the modules are described in detail as follows:
software test requirement analysis module
The software testing requirements are analyzed according to documents such as software task books, requirement specification descriptions and the like submitted by development units from two aspects of software characteristics and software scenes.
The analysis of the software features includes the following aspects:
1) basic functions of software. According to documents such as a software task book, a requirement specification and the like submitted by a developer, the functional composition and the working process of the software are comprehensively and deeply known.
2) Software cross-linking environment. Including software environments and hardware environments.
3) User type and mode of use. For flight training simulators, users are often pilots, commanders and coaches; the usage mode varies according to the user type, the purpose of use, and the like.
4) Software running state. Such as stand-alone operation, networked operation.
The analysis of the software scenario includes the following:
1) and (4) a flying environment. The flight training simulator can simulate the environment encountered during flight, such as different meteorology (blue sky, rain, snow, fog, wind), terrain (plain, mountain, basin), day and night, etc.
2) A flight failure condition. The flight personnel may need to simulate certain special flight conditions during the training process, such as fire control system faults, flight control faults, single shot failures and the like.
3) The process of launching various weapons. If the simulation of launching, guidance, flight trajectory and tactical training pod airborne of airborne air-to-air missile weapons is completed, training damage results and the like are carried out in the training task implementation stage.
4) Evasion to the flight of different missiles. It may also be desirable for a fighter pilot to train how to evade the missile using different flight techniques, such as launching jammers, infrared decoys, electronic warfare pods, etc.
5) Tactical countermeasure between aircraft. Such as a one-to-one simple air, many-to-many competition between teams, etc.
6) Tactical maneuvers. The maneuverability is one of main indexes for evaluating the performance of military aircrafts, particularly fighters, and is divided into maneuvering flight in a vertical plane, a horizontal plane and a three-dimensional space from the view of the movement track of the aircrafts. Maneuvering flight in the vertical plane mainly comprises plane flight acceleration and deceleration, dive, jump, somersault and the like; a typical action for maneuvering in the horizontal plane is horizontal hover; the maneuvering flight in three-dimensional space is commonly provided with oblique muscle fight, tactical turning, rolling, fighting half rolling and the like.
Second, software test design and implementation module
The main work of the software test design and implementation module is to establish a test environment and generate a software test case on the basis of the analyzed test requirements.
1) And establishing a test environment. Normally, the test environment should be as identical as possible to the real operating environment. If the real test environment is limited, the simulation test environment can also be used for testing, but the simulation test environment must meet the interface requirements set forth in the task book or requirements.
2) And generating a test case. Basically analyzing the test requirements, carrying out test design on the evaluation range, the evaluation items and the test input characteristics of the tested software, and compiling test cases:
① test input and test environment including hardware and software test environment;
② testing input mode and classification, wherein the input mode includes direct operation, test panel, data file, etc., and the classification includes continuity/discreteness, direct input/related test input/failure test input, etc.;
③ testing relationships between inputs, including order, concurrency, constraints, etc.;
the test case application comprises input data, test conditions, test procedures and expected results, and the test procedures in the test case comprise preparation, initialization, execution steps and end conditions of the test case. The test case set can ensure that the requirements of the specified level test on the test quality are met.
Acquiring and verifying test data in the test process; determining the execution sequence of the test cases according to the constraint conditions such as test resources, risks and the like; acquiring test resources, and developing test software if necessary; and establishing and calibrating a test environment, and performing pre-operation on a test case before test execution.
And the test instruction is reviewed, the correctness, the effectiveness and the coverage integrity of the test case are mainly reviewed, and a test organization, a test environment and related equipment tools are reviewed to be complete and meet the requirements.
Third, software testing execution module
The software test execution module mainly performs the work that a tester executes a test case on the tested software submitted by the development unit, and corresponding measures are taken according to different judgment results while test results are obtained; and checking the normal and abnormal termination conditions of the test process, and determining whether to stop the test or to modify or supplement the test case set for the test case which does not reach the test termination condition according to the check result, and further testing. The test procedure, results and discovered errors and faults are faithfully recorded during the execution.
The above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not to be construed as limiting the invention, and any modifications, equivalents, improvements and the like that fall within the spirit and principle of the present invention are intended to be included therein.
Claims (10)
1. A test method for flight training simulator software is characterized by comprising the following steps:
analyzing from two aspects of software characteristics and software scenes according to submitted software task books and requirement specification of the flight training simulator to obtain software testing requirements;
on the basis of the analyzed software test requirements, establishing a test environment and generating a software test case;
executing the test case on the submitted tested software, acquiring the test result, and taking corresponding measures according to different judgment results;
and summarizing the test process and the test result of the flight training simulator software, and giving an evaluation conclusion of the software and software quality evaluation, wherein the software quality evaluation comprises document quality evaluation and program quality evaluation.
2. A method as claimed in claim 1, wherein said analysis of the characteristics of the software comprises:
the basic software function is that the functional composition and the working process of the software are known according to a software task book and a requirement specification document submitted by a developer;
a software crosslinking environment, including a software environment and a hardware environment;
user type and mode of use;
and the software running state comprises stand-alone running and networking running.
3. A method as claimed in claim 1, wherein said analysis of the software's scenario comprises: flight environment, flight failure state, launching process of various weapons, flight evasion to different missiles, tactical countermeasure between airplanes, and tactical maneuvering.
4. The method for testing flight training simulator software of claim 1, wherein the test case comprises input data, test conditions, test procedures and expected results, and the test procedures in the test case comprise preparation, initialization, execution steps and end conditions of the test case.
5. The method for testing flight training simulator software according to claim 1, wherein the test case is executed on the submitted software to be tested, and corresponding measures are taken according to different judgment results while the test result is obtained, specifically: and checking the normal and abnormal termination conditions of the test process, and determining whether to stop the test or to modify or supplement the test case set according to the check result for the test cases which do not reach the test termination condition, and further testing.
6. A test apparatus for flight training simulator software, comprising:
the software testing requirement analysis module is used for analyzing the characteristics of software and a software scene according to the submitted flight training simulator software task book and requirement specification to obtain a software testing requirement;
the software test design and realization module is used for establishing a test environment and generating a software test case on the basis of the analyzed software test requirements;
the software test execution module executes the test case for the submitted tested software, acquires the test result and takes corresponding measures according to different judgment results;
and the software test result module is used for summarizing the test process and the test result of the flight training simulator software and giving an evaluation conclusion of the software and software quality evaluation, wherein the software quality evaluation comprises document quality evaluation and program quality evaluation.
7. The apparatus for testing flight training simulator software of claim 6, wherein the analysis of the characteristics of the software by the software testing requirement analysis module comprises:
the basic software function is that the functional composition and the working process of the software are known according to a software task book and a requirement specification document submitted by a developer;
a software crosslinking environment, including a software environment and a hardware environment;
user type and mode of use;
and the software running state comprises stand-alone running and networking running.
8. The device for testing flight training simulator software of claim 6, wherein the analysis of the software test requirement analysis module for the software scenario comprises: flight environment, flight failure state, launching process of various weapons, flight evasion to different missiles, tactical countermeasure between airplanes, and tactical maneuvering.
9. The device for testing flight training simulator software of claim 6, wherein the test cases generated by the software test design and implementation module comprise input data, test conditions, test procedures and expected results, and the test procedures in the test cases comprise preparation, initialization, execution steps and end conditions of the test cases.
10. The device for testing flight training simulator software of claim 6, wherein the software test execution module executes the test case on the submitted software to be tested, acquires the test result, and takes corresponding measures according to different determination results, specifically: and checking the normal and abnormal termination conditions of the test process, and determining whether to stop the test or to modify or supplement the test case set according to the check result for the test cases which do not reach the test termination condition, and further testing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911001001.7A CN110955592A (en) | 2019-10-21 | 2019-10-21 | Method and device for testing flight training simulator software |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911001001.7A CN110955592A (en) | 2019-10-21 | 2019-10-21 | Method and device for testing flight training simulator software |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110955592A true CN110955592A (en) | 2020-04-03 |
Family
ID=69976408
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201911001001.7A Pending CN110955592A (en) | 2019-10-21 | 2019-10-21 | Method and device for testing flight training simulator software |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110955592A (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111444106A (en) * | 2020-04-09 | 2020-07-24 | 中国人民解放军国防科技大学 | Analysis method and system for software testable requirements |
| CN111855244A (en) * | 2020-05-25 | 2020-10-30 | 青岛山景科技有限公司 | Flight simulation display system test method |
| CN112416766A (en) * | 2020-11-19 | 2021-02-26 | 北京京航计算通讯研究所 | Fault mode analysis and detection method of double-channel coupling flight control software |
| CN112462739A (en) * | 2020-11-19 | 2021-03-09 | 北京京航计算通讯研究所 | Fault detection system of double-channel coupling flight control program |
| CN112925705A (en) * | 2021-02-09 | 2021-06-08 | 上海航天控制技术研究所 | Unmanned-duty-based carrier rocket flight software acceptance method and system |
| CN113139233A (en) * | 2021-03-19 | 2021-07-20 | 徐州九鼎机电总厂 | Weapon trajectory simulation method based on immersive human-computer interaction |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102650966A (en) * | 2011-02-24 | 2012-08-29 | 王轶辰 | Multiplexing-oriented embedded software testing method and system |
| KR101387453B1 (en) * | 2012-10-24 | 2014-04-21 | 한국항공우주연구원 | Satellite flight software test bed |
| CN106383859A (en) * | 2016-08-31 | 2017-02-08 | 北京蓝天航空科技股份有限公司 | Test flight data analysis processing method |
| CN106814850A (en) * | 2016-12-03 | 2017-06-09 | 西安科锐盛创新科技有限公司 | Simulated flight operation test system and method for testing based on sight line track |
-
2019
- 2019-10-21 CN CN201911001001.7A patent/CN110955592A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102650966A (en) * | 2011-02-24 | 2012-08-29 | 王轶辰 | Multiplexing-oriented embedded software testing method and system |
| KR101387453B1 (en) * | 2012-10-24 | 2014-04-21 | 한국항공우주연구원 | Satellite flight software test bed |
| CN106383859A (en) * | 2016-08-31 | 2017-02-08 | 北京蓝天航空科技股份有限公司 | Test flight data analysis processing method |
| CN106814850A (en) * | 2016-12-03 | 2017-06-09 | 西安科锐盛创新科技有限公司 | Simulated flight operation test system and method for testing based on sight line track |
Non-Patent Citations (1)
| Title |
|---|
| 程海峰等: "民机全动飞行模拟器鉴定测试软件开发", 《计算机系统应用》 * |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111444106A (en) * | 2020-04-09 | 2020-07-24 | 中国人民解放军国防科技大学 | Analysis method and system for software testable requirements |
| CN111444106B (en) * | 2020-04-09 | 2023-09-01 | 中国人民解放军国防科技大学 | Analysis method and system for software testable requirements |
| CN111855244A (en) * | 2020-05-25 | 2020-10-30 | 青岛山景科技有限公司 | Flight simulation display system test method |
| CN112416766A (en) * | 2020-11-19 | 2021-02-26 | 北京京航计算通讯研究所 | Fault mode analysis and detection method of double-channel coupling flight control software |
| CN112462739A (en) * | 2020-11-19 | 2021-03-09 | 北京京航计算通讯研究所 | Fault detection system of double-channel coupling flight control program |
| CN112462739B (en) * | 2020-11-19 | 2021-06-29 | 北京京航计算通讯研究所 | Fault detection system of double-channel coupling flight control program |
| CN112925705A (en) * | 2021-02-09 | 2021-06-08 | 上海航天控制技术研究所 | Unmanned-duty-based carrier rocket flight software acceptance method and system |
| CN112925705B (en) * | 2021-02-09 | 2022-07-29 | 上海航天控制技术研究所 | Unmanned-duty-based carrier rocket flight software acceptance method and system |
| CN113139233A (en) * | 2021-03-19 | 2021-07-20 | 徐州九鼎机电总厂 | Weapon trajectory simulation method based on immersive human-computer interaction |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN110955592A (en) | Method and device for testing flight training simulator software | |
| US20140080099A1 (en) | Performance-Based Simulation System for an Aircraft | |
| CA3038222A1 (en) | System and method for virtual reality vehicle training field | |
| l Reweti et al. | Efficacy of low-cost PC-based aviation training devices | |
| CN109949659A (en) | A kind of flight based on Prepar3D and maintenance simulator | |
| CN114333466A (en) | Vehicle-mounted weapon verification-oriented vehicle simulator | |
| RU2250511C1 (en) | Aircraft training complex | |
| Andreev et al. | Information models for designing conceptual broad-profile flight simulators | |
| Doroftei et al. | Assessing Human Factors for Drone Operations in a Simulation Environment | |
| Koblen et al. | Selected information on flight simulators-main requirements, categories and their development, production and using for flight crew training in the both Slovak Republic and Czech Republic conditions | |
| Shashidhara et al. | Development of a Full Mission Simulator for Pilot Training of Fighter Aircraft. | |
| Wilkinson et al. | Modeling and simulation of the ship-helicopter environment | |
| Donaldson et al. | Upset simulation and training initiatives for us navy commercial derived aircraft | |
| Mądrzycki et al. | Usage of diagnostic simulator for ground engineering crew training | |
| RU111943U1 (en) | COMPREHENSIVE SIMULATOR FOR THE CREW OF THE BATTLE OF THE SHIP BASIS | |
| Perz-Osowska et al. | Usage of virtual technology in training given to ground engineering crew | |
| Andrews | Distributed simulation training for teams | |
| Gašparac | Assessment of pilot workload rating in a ship deck landing scenario | |
| Kimball | The use of simulators in the military | |
| Hall | Application of the system level airworthiness tool to the development of small electric powered UAS | |
| Conrath | Canuck pilots fly high with new simulation software | |
| McCluskey | Perspectives on simulation and miniaturization | |
| Bořil | Use of aviation simulation technologies in the Czech Air Force | |
| Sheffield et al. | Simulation Applications in V-22 and RAH-66 Design and Development | |
| Mathews | MANNED AIR COMBAT SIMULATION-A TOOL FOR DESIGN, DEVELOPMENT AND EVALUATION FOR MODERN FIGHTER WEAPON SYSTEMS AND TRAINING OF AIRCREWS |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20200403 |