CN102180271B - Pilot upper limb working space evaluation system based on work efficiency evaluation stimulation platform - Google Patents
Pilot upper limb working space evaluation system based on work efficiency evaluation stimulation platform Download PDFInfo
- Publication number
- CN102180271B CN102180271B CN2011100844092A CN201110084409A CN102180271B CN 102180271 B CN102180271 B CN 102180271B CN 2011100844092 A CN2011100844092 A CN 2011100844092A CN 201110084409 A CN201110084409 A CN 201110084409A CN 102180271 B CN102180271 B CN 102180271B
- Authority
- CN
- China
- Prior art keywords
- aviator
- upper limbs
- territory
- working space
- module
- 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.)
- Expired - Fee Related
Links
Images
Landscapes
- Management, Administration, Business Operations System, And Electronic Commerce (AREA)
Abstract
The invention provides a pilot upper limb working space evaluation system based on a work efficiency evaluation stimulation platform. The pilot upper limb working space evaluation system comprises a work efficiency evaluation stimulation platform subsystem for providing the operation for stimulating the real flight for a pilot, a 3D (three-dimensional) space coordinate location subsystem for capturing the action of the index finger tips of both hands of the pilot in the stimulated flight process, and acquiring the 3D coordinate values of the index finger tips, and a pilot upper limb working space evaluation subsystem which comprises a pilot upper limb working space calculation module, a pilot upper limb working space division module, a pilot hand 3D coordinate input module and a pilot upper limb operation domain evaluation module.
Description
Technical field
The present invention relates to the evaluation system in a kind of aviator's upper limbs operation territory, the upper limbs operation territory when the aviator carries out flight operation on the aircraft cockpit emulation platform of can testing and assessing, and then the reasonableness of test and appraisal aircraft cockpit working space layout.
Background technology
Current, the complicated flight operation to the aviator of aerial mission and flight environment of vehicle is had higher requirement.Therefore, for aviator's safety, effectively and the research of comfortable operation, become the main contents of aviation ergonomics.The unreasonable operation easier that not only increases the aviator of the layout of driving compartment working space reduces flight quality, even can influence flight safety.The aviator carries out uncomfortable operation for a long time not only can increase workload, causes physical fatigue, more can influence healthy.In order to make flight operation safety and comfort more, become the important references standard of aircraft cockpit working space layout to the upper limbs operation territory test and appraisal of aviator's flight operation in the driving compartment.On evaluating method, Chinese scholars has also been launched multinomial research.Existing research mostly is on the body biomechanics model based, extracts specific operation, and operation is analyzed like jociey stick.The method that is adopted also all is through computing formula combined with virtual emulation program, and like CATIA, driving compartment model and manikin that Jack sets up are tested and assessed.This test and appraisal are too abstract, unilateral; In true driving compartment, carry out flight operation with the aviator; The process of accomplishing aerial mission has very big difference, and therefore the confidence level of test and appraisal is limited, need verify the science that could confirm evaluation result through aviator's in the flight course in the true driving compartment practical operation; And the cost of this evaluating result through Live Flying check is very expensive, also can't reference be provided for the driving compartment working space topological design in early stage.Therefore, need a kind of approaching more true aircraft cockpit layout and aviator's practical flight method of operating to carry out the test and appraisal in aviator's upper limbs operation territory, science is credible more to make evaluating result, and can instruct the topological design of aircraft cockpit working space.
Summary of the invention
Technology of the present invention is dealt with problems and is: a kind of aviator's upper limbs operation territory evaluation system based on work efficiency test and appraisal emulation platform is provided.
Technical solution according to an embodiment of the invention is: a kind of aviator's upper limbs operation territory evaluation system based on work efficiency test and appraisal emulation platform comprises work efficiency test and appraisal emulation platform subsystem, three dimensional space coordinate positioning subsystem, aviator's upper limbs operation territory test and appraisal subsystem.Wherein, work efficiency test and appraisal emulation platform subsystem comprises flight simulation module, emulation driver's cabin module, analogue system control desk module; The three dimensional space coordinate positioning subsystem comprises data glove, three-dimensional space position tracker.Operation territory test and appraisal subsystem comprises aviator's upper limbs operation territory computing module, and module is divided in aviator's upper limbs operation territory, aviator's hand three-dimensional coordinate point load module, aviator's upper limbs operation territory test and appraisal module.
Analogue system control desk module combines the emulation driver's cabin module; Be used to set up general airliner driving compartment emulator; The emulation parts such as control wheel, button of flight operation are provided for the aviator, and to combine the flight simulation module be that the flight operation simulation provides emulation platform; The three dimensional space coordinate positioning subsystem is used for gathering action of aviator's flight simulation process both hands forefinger finger-tip operated and position three-dimensional coordinate point; Then; Reasonableness through this driving compartment working space of aviator's upper limbs operation territory test and appraisal subsystem test and appraisal instructs the working space topological design practice of driving compartment.
The present invention's advantage compared with prior art is: (1) work efficiency test and appraisal emulation platform subsystem is one and improves emulation platform that the operation of on this platform, carrying out has higher confidence level; (2) the emulation driver's cabin module in the work efficiency test and appraisal emulation platform subsystem makes up according to the size and the layout of true airliner driving compartment, combines with the analogue system control desk, and the flight operation that can make the aviator is more near practical flight; (3) the three dimensional space coordinate positioning subsystem can be caught the three-dimensional coordinate point of aviator's operation by human hand position in very short time gap (can be accurate to millisecond); And can accurately demarcate each finger, need or measure the defective that just can obtain coordinate points through mathematical computations before having avoided.The three dimensional space coordinate positioning subsystem combines work efficiency test and appraisal emulation platform subsystem can obtain thousands of coordinate points, for test and appraisal provide a large amount of accurate data, has improved the accuracy of test and appraisal; (4) test and appraisal subsystem in aviator's upper limbs operation territory has adopted the method that the operation by human hand position three-dimensional coordinate point of aviator's body biomechanics model and the acquisition of aviator's flight simulation compares, and theory and practice is well combined.(5) adopt the present invention to instruct, shortened the lead time effectively, reduce design cost in the initial stage of aircraft cockpit working space topological design.
According to an aspect of the present invention, a kind of aviator's upper limbs operation territory evaluation system based on work efficiency test and appraisal emulation platform is provided, has it is characterized in that comprising:
Work efficiency test and appraisal emulation platform subsystem is used to provide the flight simulation operating environment;
The three dimensional space coordinate positioning subsystem is used for gathering aviator's both hands forefinger finger tip D coordinates value in the flight simulation process;
Test and appraisal subsystem in aviator's upper limbs operation territory is used for driving compartment working space layout is tested and assessed.
Description of drawings
Fig. 1 is the constructional drawing of the evaluation system in aviator's upper limbs operation according to an embodiment of the invention territory.
Fig. 2 is an emulation driver's cabin module constructional drawing according to an embodiment of the invention.
Fig. 3 is aviator's upper limbs operation according to an embodiment of the invention territory evaluation and test subsystem work diagram of circuit.
Fig. 4 is aviator's body biomechanics illustraton of model according to an embodiment of the invention.
Fig. 5 A-Fig. 5 C is aviator's upper limbs operation according to an embodiment of the invention territory test and appraisal examples of interfaces figure.
The specific embodiment
As shown in Figure 1, the evaluation system in aviator's upper limbs operation according to an embodiment of the invention territory comprises work efficiency test and appraisal emulation platform subsystem (1), three dimensional space coordinate positioning subsystem (2), aviator's upper limbs operation territory test and appraisal subsystem (3).
Aviator's upper limbs operation according to an embodiment of the invention territory test and appraisal subsystems (3) comprise aviator's upper limbs operation territory computing module (31); Module (32) is divided in aviator's upper limbs operation territory; Aviator's hand three-dimensional coordinate point load module (33), aviator's upper limbs operation territory test and appraisal module (34).
In instantiation according to an embodiment of the invention, aviator's upper limbs operation territory test and appraisal subsystems (3) are by the Matal software programming, and its exemplary interfaces is shown in Fig. 5 A to Fig. 5 C.Workflow according to an embodiment of the invention is as shown in Figure 3, and wherein aviator's upper limbs operation territory computing module (31) is to derive aviator's upper limbs operation territory computing formula by aviator's body biomechanics model.
In one embodiment of the invention, used the work efficiency test and appraisal emulation platform subsystem of prior art.Work efficiency test and appraisal emulation platform subsystem comprises flight simulation module, emulation driver's cabin module, analogue system control desk module.
Flight simulation module according to an embodiment of the invention comprises flight control submodule, fuel oil submodule, hydraulic subsidiary module, alighting gear submodule.The primary control circuit of flight control submodule emulation aircraft and the work-based logic and the system performance of secondary control system comprise roll manipulation, pitch control etc.; The fuel oil submodule carries out emulation to the work-based logic and the system performance of fuel oil system, mainly comprises oil mass indicating system and fuel oil system of distribution etc.; The hydraulic subsidiary module is mainly carried out emulation to the work-based logic and the system performance of hydraulic efficiency pressure system, for functions such as operation of landing gear, operation of landing flaps provide simulate signal; The alighting gear submodule is mainly realized the work-based logic and the system performance of main landing gear, nose-gear, to support the Landing Gear System normal operation.Landing-gear actuation is provided with realization in the control desk system.
The structure of emulation driver's cabin module according to an embodiment of the invention is as shown in Figure 2, and the driving compartment display and control panel topmost is an emulation part anti-dazzle device.3 multi-functional demonstration (MFD have side by side arranged below the emulation part anti-dazzle device; Multi-Function Display) liquid crystal display; What be positioned at the driving compartment left part is an emulation part control wheel and an emulation part seat; A liquid crystal display that is used to show 19 cun multi-functional demonstrations (MFD) of flight information has been placed on the left side; Right part be a signal part control wheel and signal part seat, two control wheel intermediate arrangement the touch-screen of 19 inches multi-functional demonstrations (MFD, Multi-Function Display).The aviator realizes aircraft roll and pitching through handling emulation part control wheel mechanism controls aileron and elevating rudder.Left (conter clockwise), when (cw) rotates control wheel to the right, aileron movement is realized aircraft roll control; Push away, when drawing jociey stick, control elevating rudder deflection, thereby realize vertical pitch control of aircraft.
Analogue system control desk module possesses following function: system freezes, system reset and exit function; To the alighting gear operating function; The state sampling function, through reading the sampling file, the state when making system recovery arrive file storage possesses three state sampling of taking off, cruise, land at least; Call the function of work efficiency test and appraisal program, for work efficiency test and appraisal program reserve speed, highly, gesture interface, the relevant flying quality of output is to carry out the work efficiency test and appraisal.
In one embodiment of the invention; Used the three dimensional space coordinate position fixing system of prior art; Comprise data glove and three-dimensional space position tracker; Data glove is the main interactive device of virtual reality applications, can carry out grasping body, moves, assembles, handles, control, and the branch of the left hand and the right hand is arranged.Data glove comprises the light transmitting fiber that is fixed on the elastic fibre gloves and the three-dimensional tracking transducer of belt, at the joint of every finger a light transmitting fiber ring is arranged. optical fiber becomes several by plastic tube bundle, to adapt to the curvilinear movement of finger.The three-dimensional space position tracker is the device that is used for the space track and localization, generally is used in combination with data glove, can follow the tracks of with the output data gloves in the position of sensor.In instantiation according to an embodiment of the invention; Adopted the Shapehand data glove of Canadian Measurand company; Flock of birds tracker (Flock of Birds) in conjunction with Ascension company; The three-dimensional coordinate point of both hands forefinger finger tip when the seizure aviator carries out the simulated flight operation, the D coordinates value of point is caught in output.
As shown in Figure 4, aviator's body biomechanics model according to an embodiment of the invention is reduced to lever hinge mechanism with human body; This model is placed the simulator cockpit hardware module, is that initial point is set up three dimensional space coordinate system with potential reference point in the chair surface.In according to one embodiment of present invention, trunk is set one degree of freedom, and around the rotation of Y axle, α is an angle of body, is the angle of trunk and Z axle, and angle of body is for bearing when receding, and angle of body is for just when turning forward.Aviator's upper limbs operation territory is the scope that finger tip can touch under the arm straight configuration; Adopt the forefinger finger tip among the present invention; Therefore; Regard aviator's upper arm, forearm and finger total length as straight line around shoulder joint Node B, C, the site is to rotate during the three dimensional space coordinate of initial point is in seat.On each contour plane, the intrinsic curve in upper limbs operation territory is for being the circular arc in the center of circle with the shoulder joint, and its expression formula can be found the solution in the three dimensional space coordinate system that sets up.
The proportionate relationship of the table 1 Chinese adult male sex each link of upper limbs and height
| The body section | Whole body | Neck | Trunk | Shoulder breadth | Upper arm | Forearm | Hand |
| Length | L | 0.19L | 0.29L | 0.224L | 0.19L | 0.14L | 0.11L |
Derive the proportionate relationship of each spot size of aviator and height L according to the anthropological measuring basic data in the GB10000-88 standard, see table 1, the computing formula of trying to achieve aviator's upper limbs operation territory with geometric method is following:
Module (32) is divided in aviator's upper limbs operation territory in the aviator's upper limbs operation territory test and appraisal subsystems (3), with reference to the relevant criterion among HB6154-88 and the GJB35B-2008, aviator's upper limbs operation territory is divided into three zones.First zone is comfortable territory, promptly when aviator's sitting posture that keeps cruising, and during α=-15 °, the zone that both hands forefinger finger tip can reach and operate under the arm nature stretching, extension situation; Second zone is that function can reach the territory, promptly when aviator's sitting posture that keeps cruising, and during α=-15 °, under arm and the shoulder muscle maximum extension situation, the zone that both hands forefinger finger tip can arrive and operate, second area is than the first area 50mm that stretches out; The 3rd zone can reach the territory for maximum, promptly keeps cruising sitting posture as the aviator, during α=35 °, and the zone that both hands forefinger finger tip can reach and operate under the natural stretching, extension situation of arm.Zone in the driving compartment beyond the upper limbs operation territory is the 4th zone, is the inaccessiable zone of aviator's upper limbs, promptly non-operation territory.
Aviator's hand three-dimensional coordinate point load module (33) in aviator's upper limbs operation territory test and appraisal subsystems (3) is an interface module, and three coordinate points of aviator's both hands forefinger finger tip that are used for three dimensional space coordinate positioning subsystem (2) is collected are with text formatting input aviator upper limbs operation territory test and appraisal subsystem (3).
Aviator's upper limbs operation territory test and appraisal modules (34) in aviator's upper limbs operation territory test and appraisal subsystems (3) combine aviator's upper limbs operation territory computing module (31), aviator's upper limbs operation territory to divide (32) two parts of module and test and assess, and the test and appraisal flow process is following:
(1) aviator's height of flight simulation is carried out in input, generates the three-dimensional envelope diagram in aviator's upper limbs operation territory according to aviator's upper limbs operation domain classification method, three dimensional space is divided into comfortable territory, function can reach the territory, maximum can reach territory, four zones, non-operation territory.
(2) aviator's operation by human hand position three-dimensional coordinate point of gathering in the input flight simulation process calculates the percentum λ that drops on each regional internal coordinate point respectively
i, comfortable territory is λ
1, it is λ that function can reach the territory
2, it is λ that maximum can reach the territory
3, non-operation territory is λ
4
(3) judge λ
iValue, carry out the test and appraisal of the rationally distributed property of this driving compartment working space, test and appraisal scale in aviator's upper limbs operation territory is seen table 2.λ
4>0 o'clock, grade was a V, and the working space layout is very poor; λ
4=0 o'clock, if λ
3>30%, grade is an IV, and the working space layout is relatively poor; λ
4=0 o'clock, if 0<λ
3≤30%, grade is an III, and the working space layout is poor slightly; λ
3=0 o'clock, if λ
2>30%, grade is an II, and the working space layout is better; λ
3=0 o'clock, if λ
2≤30%, grade is an I, and the working space layout is good.Finally judge, draw evaluating result according to above evaluation standard.Evaluating result embodies with image and document format, can export and preserve.
Table 2 aviator upper limbs operation territory test and appraisal scale
Claims (3)
1. aviator's upper limbs operation territory evaluation system based on work efficiency test and appraisal emulation platform is characterized in that comprising:
Work efficiency test and appraisal emulation platform subsystem (1) is used to provide the flight simulation operating environment;
Three dimensional space coordinate positioning subsystem (2) is used for gathering aviator's both hands forefinger finger tip D coordinates value in the flight simulation process;
Test and appraisal subsystem (3) in aviator's upper limbs operation territory is used for driving compartment working space layout is tested and assessed,
Wherein said work efficiency test and appraisal emulation platform subsystems (1) comprising:
Flight simulation module (11) is used for flight control system, fuel oil system, the hydraulic efficiency pressure system to aircraft, the simulation of Landing Gear System characteristic;
Emulation driver's cabin module (12) is used to provide the working space layout of true airliner driving compartment, and the hardware device of simulated flight is provided;
Analogue system control desk module (13) is used for the function such as control, state sampling, data output to system,
Said three dimensional space coordinate positioning subsystem (2) comprising:
Data glove, the operational motion of hand forefinger finger tip when being used to catch aviator's flight simulation;
The three-dimensional space position tracker is used to locate and the position of both hands forefinger finger tip when exporting aviator's flight simulation,
Said aviator's upper limbs operation territory test and appraisal subsystems (3) comprising:
Aviator's upper limbs operation territory computing module (31) is used to calculate the three-dimensional envelope diagram in aviator's upper limbs operation territory;
Module (32) is divided in aviator's upper limbs operation territory, is used for the driving compartment working space is divided;
Aviator's hand three-dimensional coordinate point load module (33) is used for comparing with the scope in aviator's upper limbs operation territory;
Test and appraisal module (34) in aviator's upper limbs operation territory is used for driving compartment working space layout is tested and assessed.
2. the aviator's upper limbs operation territory evaluation system based on flight simulation as claimed in claim 1 is characterized in that described aviator's upper limbs operation territory computing module (31) comprising:
It is the part that initial point is set up three dimensional space coordinate system with the seat potential reference point that aviator's body biomechanics model is placed the simulator cockpit hardware module;
Setting section is used to set trunk and has only one degree of freedom, and around Y axle rotation, α is an angle of body, is the angle of trunk and Z axle, and angle of body is for bearing when receding, and angle of body is for just when turning forward;
Calculating section is used for the proportionate relationship according to each spot size of aviator and height L, tries to achieve the computing formula in aviator's upper limbs operation territory with geometric method:
3. the aviator's upper limbs operation territory evaluation system based on flight simulation as claimed in claim 1 is characterized in that aviator's upper limbs operation territory test and appraisal modules (34) are used to carry out following operation:
(1) aviator's height of flight simulation is carried out in input, and call aviator's upper limbs operation territory and divide the three-dimensional envelope diagram in module generation aviator upper limbs operation territory,
(2) call aviator's hand three-dimensional coordinate point load module, calculate the percentum λ that drops on each regional internal coordinate point
i, said zone comprises comfortable territory λ
1, function can reach territory λ
2, maximum can reach territory λ
3, non-operation territory λ
4,
(3) judge λ
iValue, carry out the test and appraisal of the rationally distributed property of this driving compartment working space, wherein:
λ
4>0 o'clock, grade was a V, and the working space layout is very poor;
λ
4=0 o'clock, if λ
3>30%, grade is an IV, and the working space layout is relatively poor;
λ
4=0 o'clock, if 0<λ
3≤30%, grade is an III, and the working space layout is poor slightly;
λ
3=0 o'clock, if λ
2>30%, grade is an II, and the working space layout is better;
λ
3=0 o'clock, if λ
2≤30%, grade is an I, and the working space layout is good.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011100844092A CN102180271B (en) | 2011-04-05 | 2011-04-05 | Pilot upper limb working space evaluation system based on work efficiency evaluation stimulation platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011100844092A CN102180271B (en) | 2011-04-05 | 2011-04-05 | Pilot upper limb working space evaluation system based on work efficiency evaluation stimulation platform |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN102180271A CN102180271A (en) | 2011-09-14 |
| CN102180271B true CN102180271B (en) | 2012-12-26 |
Family
ID=44566607
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011100844092A Expired - Fee Related CN102180271B (en) | 2011-04-05 | 2011-04-05 | Pilot upper limb working space evaluation system based on work efficiency evaluation stimulation platform |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102180271B (en) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107219928A (en) * | 2017-06-23 | 2017-09-29 | 西安天圆光电科技有限公司 | The equipment data acquisition analyzing and method of a kind of opportunity of combat pilot operator identification |
| CN107274747A (en) * | 2017-08-01 | 2017-10-20 | 中国航空工业集团公司西安飞机设计研究所 | A kind of aircraft cockpit ergonomic assessment system |
| CN109145485B (en) * | 2018-09-04 | 2023-08-04 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | Man-machine efficiency testing method and system |
| CN112560198B (en) * | 2020-12-21 | 2023-01-31 | 北京航空航天大学 | Activity domain subdivision method for measuring human upper limb operation work efficiency |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2005044150A (en) * | 2003-07-23 | 2005-02-17 | Sony Corp | Data collecting device |
| AU2010292270A1 (en) * | 2009-09-08 | 2012-04-12 | Aerovironment, Inc. | Electric vehicle simulator and analyzer (EVSA) for electric vehicle supply equipment |
-
2011
- 2011-04-05 CN CN2011100844092A patent/CN102180271B/en not_active Expired - Fee Related
Non-Patent Citations (11)
| Title |
|---|
| JP特开2005-44150A 2005.02.17 |
| 基于动力学模型的飞行员舒适操作域研究;王睿等;《计算机仿真》;20060831;第23卷(第08期);全文 * |
| 基于舒适性分析的舱室手操纵装置优化布局;王睿等;《兵工学报》;20080930;第29卷(第9期);全文 * |
| 应用虚拟现实技术的人机交互仿真系统开发;曹文钢等;《工程图学学报》;20100228(第1期);全文 * |
| 张磊等.飞机座舱人机工效评定实验台研制.《飞行力学》.2009,第27卷(第1期),全文. |
| 曹文钢等.应用虚拟现实技术的人机交互仿真系统开发.《工程图学学报》.2010,(第1期),全文. |
| 王丽荣等.飞机拨动开关布置的人机工效分析.《中国民航飞行学院学报》.2004,第15卷(第2期),全文. |
| 王睿等.基于动力学模型的飞行员舒适操作域研究.《计算机仿真》.2006,第23卷(第08期),全文. |
| 王睿等.基于舒适性分析的舱室手操纵装置优化布局.《兵工学报》.2008,第29卷(第9期),全文. |
| 飞机座舱人机工效评定实验台研制;张磊等;《飞行力学》;20090228;第27卷(第1期);全文 * |
| 飞机拨动开关布置的人机工效分析;王丽荣等;《中国民航飞行学院学报》;20040331;第15卷(第2期);全文 * |
Also Published As
| Publication number | Publication date |
|---|---|
| CN102180271A (en) | 2011-09-14 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Ajanic et al. | Bioinspired wing and tail morphing extends drone flight capabilities | |
| CN102180271B (en) | Pilot upper limb working space evaluation system based on work efficiency evaluation stimulation platform | |
| CN102693349B (en) | Pilot attention distribution work efficiency evaluation system and method based on airplane cockpit display interface | |
| Harvey et al. | Gull-inspired joint-driven wing morphing allows adaptive longitudinal flight control | |
| CN104573285A (en) | Method for designing layout of cockpit according to action characteristics of pilot | |
| CN114090006A (en) | System and method for evaluating man-machine interface layout of civil aircraft cockpit | |
| CN107741300A (en) | A kind of center of gravity of airplane instruction device | |
| da Silva et al. | Comparison of anthropometry of Brazilian and US Military population for flight deck design | |
| CN113460328A (en) | System and method for civil aircraft ground comprehensive dynamic detection | |
| Jiang et al. | Transformer network intelligent flight situation awareness assessment based on pilot visual gaze and operation behavior data | |
| CN109543297A (en) | A kind of modification method of airframe to ejector seat aerodynamic interference | |
| Datta | Fundamental understanding, prediction and validation of rotor vibratory loads in steady-level flight | |
| Allerton | Flight Simulation-past, present and future | |
| CN102629139A (en) | Ground effect flight management system for ground effect vehicle | |
| Jianlin et al. | Progress of Chinese “Dove” and Future Studies on Flight Mechanism of Birds and Application System. | |
| Brickman et al. | Haptic specification of environmental events: Implications for the design of adaptive, virtual interfaces | |
| Claus et al. | DES turbulence modelling on the c-130 comparison between computational and experimental results | |
| Gennaretti et al. | Acoustic prediction of helicopter unsteady manoeuvres | |
| Litaker et al. | NASA’s Ground Test Unit (GTU) Lunar Terrain Vehicle (LTV) Conceptual Hand Controllers Studies | |
| Edwards | Analysis of three-dimensional separated flow using interacting boundary-layer theory | |
| de Paula et al. | Aerodynamic Longitudinal Coefficient Modeling During Aircraft Design Phases | |
| Suresh et al. | Dynamic Landing Response Analysis of a Flexible Tailless Delta Wing Aircraft. | |
| Zhang et al. | Handling Quality Evaluation Method in Aircraft Cockpit Based on Pilot Performance | |
| Ren et al. | Eye movement analysis of cockpit interface of small aircraft under the airfield traffic pattern | |
| RU2006131472A (en) | PERSONAL VIRTUAL PILOT SIMULATOR |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20121226 Termination date: 20150405 |
|
| EXPY | Termination of patent right or utility model |