CN203733342U - Commanding and monitoring device suitable for flight simulator - Google Patents
Commanding and monitoring device suitable for flight simulator Download PDFInfo
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- CN203733342U CN203733342U CN201420053303.5U CN201420053303U CN203733342U CN 203733342 U CN203733342 U CN 203733342U CN 201420053303 U CN201420053303 U CN 201420053303U CN 203733342 U CN203733342 U CN 203733342U
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Abstract
The utility model belongs to the flight simulation technical field and relates to a commanding and monitoring device suitable for a flight simulator. According to the commanding and monitoring device, a four-path hard disk video recorder capable of simultaneously receiving Vadio signals and/or VGA/DVI signals is selected; the output end of the hard disk video recorder is connected with a display terminal through using a VGA/DVI signal line; and either a single projection display unit or a display on an instructor stage can be selected as the display terminal. With the commanding and monitoring device adopted, required information can be obtained visually and conveniently; a variety of related data information of aircrafts in simulated training can be known selectively in real time; and subjective and objective information of trainees can be observed in real time. The commanding and monitoring device can be conveniently applied to development and simulation tactical confrontation networking.
Description
Technical field
The utility model belongs to flight simulation technology field, is specifically related to a set of command and monitor device that is applicable to flight simulator.
Background technology
Conventionally in fly simulation training and imitated tactic training, all should there is teacher participant is supervised and guided and pass judgment on, teacher also needs to play the part of the roles such as commander, ground blank pipe or warning message simultaneously, the uncertainty of the human intervention task story of a play or opera, thus increase fidelity and the difficulty of training.These just need teacher can grasp real-time and accurately attitude, operation logic, action details, the Automobile driving situation of participant, can monitor technology, the tactics information such as status data, position data, inter-related task system data of aircraft simultaneously.
For ensureing the demand, conventionally there are two kinds of ways:
1 carries out real time record by network technology means by whole technical parameters in training process, then these parameter informations is reappeared out on corresponding monitor scope.Realize the method higher to computer hardware requirement; And in the record data of magnanimity, be not easy to teacher and make in time rapidly differentiation; The method cannot provide participant subjective information simultaneously.
2 install multiple cameras in simulator, and in the facial expression to participant, bimanualness and cabin, each display and instrument are taken respectively, carry out the collection of above-mentioned teacher's demand information by picture.Although the method has been taken into account the collection of participant subjective information and objective information, owing to being guiding according to the Automobile driving of participant completely, the objective data obtaining is limited.And for collecting information accurately as far as possible comprehensively, multiple cameras are erected in simulator, havoc fidelity and the feeling of immersion of simulator entirety, participant is placed oneself in the midst of in film studio seemingly.
Said method cuts both ways, but all can not in simulated training, effectively meet teacher's demand.
Summary of the invention
The purpose of this utility model is to provide a set of command and monitor device that is applicable to flight simulator, effectively meets the demand of teacher in simulated training.
For achieving the above object, technical solution adopted in the utility model is:
Be applicable to a command and monitor device for flight simulator, this device selects 4 tunnels can receive the DVR of Vadio signal and/or VGA/DVI signal simultaneously; The output terminal of DVR is connected with display terminal with VGA/DVI signal wire; Display terminal can be selected independent projection display unit, also can use the upper display of instructor station.
Described device is selected under a low-light (level) environment pinhole camera and camera lens that can self-adaptation work, as subjective informations such as facial camera collection participant facial expressions; Facial camera is arranged on near flat aobvious or front panel top in passenger cabin, towards participant head; Picture debugging is to can clearly distinguishing participant expression; According to simulator erecting stage conditioned measurement from camera installation site in simulator to pulpit in the length of DVR installation site, No. 1 input interface of the 75 Ω monitor video Xian Jiangci road vision signals access DVR by corresponding length; Utilize the Audio Data Line of corresponding length that the audio output of video camera is connected to audio amplifier, can monitor the aural information and the sound warning information that in passenger cabin, produce; Audio amplifier can share with instructor station's system.
Described device is selected under a low-light (level) environment video camera and wide-angle lens that can self-adaptation work, as in overall camera collection simulator taking passenger cabin and what comes into a driver's primary vision area as the 3rd main visual angle picture information; Overall camera is arranged on to slightly high position, simulator porch, towards passenger cabin dead ahead; Picture, taking what comes into a driver's primary vision area as main, is taken into account passenger cabin front upper part; According to simulator erecting stage conditioned measurement from camera installation site in simulator to pulpit in the length of DVR installation site, No. 2 input interfaces of the 75 Ω monitor video Xian Jiangci road vision signals access DVR by corresponding length.
Described device accesses the head-up display image information from external system No. 3 input interfaces of DVR by VGA/DVI video signal cable; The comprehensive degree of head-up display image information is higher, can help teacher to understand in real time the situation that participant the first visual angle faces.
Described device selects the frequency switch of one 4 input 1 output that other main image information from external system (navigation screen, state of flight picture, engine parameter picture and air intelligence situation picture) is connected with the input end of video switcher by VGA/DVI video signal cable respectively, the output terminal of video switcher is connected to No. 4 input interfaces of DVR by VGA/DVI video signal cable.
The obtained beneficial effect of the utility model is:
(1) can obtain to intuitive and convenient required information
On instructor station, can intensively observe the information that can differentiate participant physical training condition, these information are relatively with conspicuous characteristics, and operation is controlled simple, is incorporated in a display terminal.
(2) subjectivity, objective information that can Real Time Observation participant
Comprise operation logic, action details, the Automobile driving situation of participant, the variation of mood, attitude while even undergoing training.Can understand in real time the integrated information at participant the first visual angle, simultaneously can be according to the disposal situation of the 3rd view participant.
(3) can real-time selection ground understand the various related data information of aircraft in simulated training
According to different training missions, grasp the data message under aircraft different mode different phase, to differentiate the level of training of participant.
(4) be convenient to expand and apply in the networking of simulation tactical confrontation
Can be applicable in multiple flight simulator simulated training, convenient application in many simulator tactical confrontation networkings, even for simulated training Command Tactical provides information support.
Brief description of the drawings
Fig. 1 is the command and monitor structure drawing of device that is applicable to flight simulator described in the utility model.
Embodiment
Below in conjunction with the drawings and specific embodiments, the utility model is elaborated.
As shown in Figure 1, the command and monitor device that is applicable to flight simulator described in the utility model selects 4 tunnels can receive the DVR of Vadio signal and/or VGA/DVI signal simultaneously.The output terminal of DVR is connected with display terminal with VGA/DVI signal wire.
Display terminal can be selected independent projection display unit, also can use the upper display of instructor station.
Select under a low-light (level) environment can self-adaptation work pinhole camera and camera lens, as subjective informations such as facial camera collection participant facial expressions.Facial camera is arranged on near flat aobvious or front panel top (can not obviously affect layout and the outward appearance of existing equipment in cabin) in passenger cabin, towards participant head.Picture debugging is to can clearly distinguishing participant expression.According to simulator erecting stage conditioned measurement from camera installation site in simulator to pulpit in the length of DVR installation site, No. 1 input interface of the 75 Ω monitor video Xian Jiangci road vision signals access DVR by corresponding length.Utilize the Audio Data Line of corresponding length that the audio output of video camera is connected to audio amplifier, can monitor the aural information and the sound warning information that in passenger cabin, produce.Audio amplifier can share with instructor station's system.
Select under a low-light (level) environment can self-adaptation work video camera and wide-angle lens, as in overall camera collection simulator taking passenger cabin and what comes into a driver's primary vision area as the 3rd main visual angle picture information.Overall camera is arranged on to slightly high position, simulator porch, towards passenger cabin dead ahead.Picture should, taking what comes into a driver's primary vision area as main, be taken into account passenger cabin front upper part.According to simulator erecting stage conditioned measurement from camera installation site in simulator to pulpit in the length of DVR installation site, No. 2 input interfaces of the 75 Ω monitor video Xian Jiangci road vision signals access DVR by corresponding length.
Head-up display image information from external system is accessed to No. 3 input interfaces of DVR by VGA/DVI video signal cable.Because the comprehensive degree of head-up display image information is higher, and can help teacher to understand in real time the situation that participant the first visual angle faces.
Select the video switcher of one 4 input 1 output.Other main image information from external system (navigation screen, state of flight picture, engine parameter picture and air intelligence situation picture) is connected with the input end of video switcher by VGA/DVI video signal cable respectively, the output terminal of video switcher is connected to No. 4 input interfaces of DVR by VGA/DVI video signal cable.
Claims (5)
1. a set of command and monitor device that is applicable to flight simulator, is characterized in that: this device selects 4 tunnels can receive the DVR of Vadio signal and/or VGA/DVI signal simultaneously; The output terminal of DVR is connected with display terminal with VGA/DVI signal wire; Display terminal is selected independent projection display unit, uses the upper display of instructor station.
2. the command and monitor device that is applicable to flight simulator according to claim 1, it is characterized in that: described device is selected under a low-light (level) environment pinhole camera and camera lens that can self-adaptation work, as facial camera collection participant facial expression subjective information; Facial camera is arranged on near flat aobvious or front panel top in passenger cabin, towards participant head; Picture debugging is to can clearly distinguishing participant expression; According to simulator erecting stage conditioned measurement from camera installation site in simulator to pulpit in the length of DVR installation site, No. 1 input interface of the 75 Ω monitor video Xian Jiangci road vision signals access DVR by corresponding length; Utilize the Audio Data Line of corresponding length that the audio output of video camera is connected to audio amplifier, can monitor the aural information and the sound warning information that in passenger cabin, produce; Audio amplifier and instructor station's system share.
3. the command and monitor device that is applicable to flight simulator according to claim 1, it is characterized in that: described device is selected under a low-light (level) environment video camera and wide-angle lens that can self-adaptation work, as in overall camera collection simulator taking passenger cabin and what comes into a driver's primary vision area as the 3rd main visual angle picture information; Overall camera is arranged on to slightly high position, simulator porch, towards passenger cabin dead ahead; Picture, taking what comes into a driver's primary vision area as main, is taken into account passenger cabin front upper part; According to simulator erecting stage conditioned measurement from camera installation site in simulator to pulpit in the length of DVR installation site, No. 2 input interfaces of the 75 Ω monitor video Xian Jiangci road vision signals access DVR by corresponding length.
4. the command and monitor device that is applicable to flight simulator according to claim 1, is characterized in that: described device accesses the head-up display image information from external system No. 3 input interfaces of DVR by VGA/DVI video signal cable.
5. the command and monitor device that is applicable to flight simulator according to claim 1, it is characterized in that: described device selects the frequency switch of one 4 input 1 output by the main image information from external system, comprise that navigation screen, state of flight picture, engine parameter picture and air intelligence situation picture are connected with the input end of video switcher by VGA/DVI video signal cable respectively, the output terminal of video switcher is connected to No. 4 input interfaces of DVR by VGA/DVI video signal cable.
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Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105912975A (en) * | 2015-02-20 | 2016-08-31 | 空中客车集团印度私人有限公司 | Management of aircraft in-cabin activities occuring during turnaround using video analytics |
CN107396058A (en) * | 2017-08-23 | 2017-11-24 | 芜湖超源力工业设计有限公司 | A kind of special fly simulation training supervising device of space flight |
CN108107825A (en) * | 2017-11-30 | 2018-06-01 | 江西洪都航空工业集团有限责任公司 | A kind of Aircraft Simulator automatic control system |
CN109473012A (en) * | 2018-12-20 | 2019-03-15 | 北京中航科电测控技术股份有限公司 | A kind of manipulation force feedback system for simulated flight |
-
2014
- 2014-01-27 CN CN201420053303.5U patent/CN203733342U/en not_active Expired - Fee Related
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105912975A (en) * | 2015-02-20 | 2016-08-31 | 空中客车集团印度私人有限公司 | Management of aircraft in-cabin activities occuring during turnaround using video analytics |
CN107396058A (en) * | 2017-08-23 | 2017-11-24 | 芜湖超源力工业设计有限公司 | A kind of special fly simulation training supervising device of space flight |
CN108107825A (en) * | 2017-11-30 | 2018-06-01 | 江西洪都航空工业集团有限责任公司 | A kind of Aircraft Simulator automatic control system |
CN109473012A (en) * | 2018-12-20 | 2019-03-15 | 北京中航科电测控技术股份有限公司 | A kind of manipulation force feedback system for simulated flight |
CN109473012B (en) * | 2018-12-20 | 2019-12-17 | 北京中航科电测控技术股份有限公司 | control force feedback system for simulating flight |
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C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20140723 Termination date: 20170127 |