CN112767791A - Simulated aviation clock system developed for flight simulator and operation method thereof - Google Patents
Simulated aviation clock system developed for flight simulator and operation method thereof Download PDFInfo
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- 238000000034 method Methods 0.000 title claims abstract description 21
- 238000004088 simulation Methods 0.000 claims abstract description 38
- 238000005259 measurement Methods 0.000 claims abstract description 37
- 230000004044 response Effects 0.000 claims abstract description 11
- 238000006243 chemical reaction Methods 0.000 claims abstract description 6
- 238000007689 inspection Methods 0.000 claims abstract description 5
- 238000009825 accumulation Methods 0.000 claims description 3
- 238000012937 correction Methods 0.000 claims description 3
- 230000003993 interaction Effects 0.000 abstract description 3
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- 238000012549 training Methods 0.000 description 6
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- 230000007812 deficiency Effects 0.000 description 2
- 239000004973 liquid crystal related substance Substances 0.000 description 2
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- 230000009286 beneficial effect Effects 0.000 description 1
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- G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
- G09B19/00—Teaching not covered by other main groups of this subclass
- G09B19/12—Clock-reading
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- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
- G09B9/00—Simulators for teaching or training purposes
- G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
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Abstract
The invention discloses a simulation aviation clock system developed aiming at a flight simulator and an operation method thereof, wherein the simulation aviation clock system comprises: the power-on module is used for realizing voltage conversion and carrying out power-on inspection on the interior of the system; the fault analysis response module is used for capturing the fault state of the system and analyzing to realize corresponding response; the brightness adjusting module is used for adjusting the brightness of the simulation display in the system hardware instrument; the current calculating module is used for calculating current time; the time measurement calculating module is used for realizing a timing function; the time of flight resolving module is used for calculating the time of flight and calculating the accumulated value of the time of flight; and the reset resolving module is used for realizing reset and reset of the system. Has the advantages that: the system function is realized by software and upper computer data interaction to control a hardware instrument, so that the structure of the simulation aviation clock is similar to a real aviation clock, and the operation mode is consistent with that of a real aircraft aviation clock.
Description
Technical Field
The invention relates to the technical field of aviation clocks, in particular to a simulation aviation clock system developed aiming at a flight simulator and an operation method thereof.
Background
During the flight of an aircraft, the pilot needs to know not only the standard time but also the time when the aircraft has finished flying. The common clock can only display standard time but cannot measure the aviation flight time, and the timing device capable of recording the time period cannot display the standard time, so that a lot of troubles are brought to aviation flight. The aviation clock is used for overcoming the defects of the technical problems, not only can display standard time during navigation, but also can measure the flying time of an aircraft, and is accurate in timing and convenient to use.
It is necessary to undergo a long and rigorous training process before the aircraft pilot goes on duty to pilot the aircraft. Simulating the driving of an aircraft in an aviation flight simulator is an important element in pilot training disciplines. The training includes the mastering and use of an aircraft clock. Therefore, a simulated aviation clock is required to be developed for the special environment of the airplane simulator so as to meet the requirement of aviation training.
An effective solution to the problems in the related art has not been proposed yet.
Disclosure of Invention
The present invention is directed to a simulated aircraft clock system developed for a flight simulator and a method of operating the same, which overcome the above-mentioned problems of the prior art.
Therefore, the invention adopts the following specific technical scheme:
according to one aspect of the invention, there is provided a simulated aircraft clock system developed for a flight simulator, the simulated aircraft clock system comprising:
the power-on module is used for realizing voltage conversion and carrying out power-on inspection on the interior of the system;
the fault analysis response module is used for capturing the fault state of the system and analyzing to realize corresponding response;
the brightness adjusting module is used for adjusting the brightness of the simulation display in the system hardware instrument;
the current calculating module is used for calculating current time;
the time measurement calculating module is used for realizing a timing function;
the time of flight resolving module is used for calculating the time of flight and calculating the accumulated value of the time of flight;
and the reset resolving module is used for realizing reset and reset of the system.
Furthermore, the simulation aviation clock system is electrically connected with the cabin simulation system, the electromechanical system, the flight system, the instructor platform system and the cabin simulation subsystem in sequence.
Furthermore, the cabin simulation system provides onboard personnel operation information and illumination for the simulation aviation clock system, and the simulation aviation clock system provides the current time, timing and navigation time for the cabin simulation subsystem.
Further, the electromechanical system provides a power supply signal for the simulated aviation clock system.
Further, the flight system provides a landing gear lift-off signal for the simulated aviation clock system.
Further, the instructor station system provides simulated fault information for the simulated aviation clock system.
According to another aspect of the invention, an operation method of the simulated aviation clock system developed for the flight simulator is further provided, which is used for realizing the operation of the simulated aviation clock system developed for the flight simulator, wherein a hardware instrument of the simulated aviation clock system is provided with a brightness button, a reset button, a menu button, a time measurement button and a display, and is used for realizing specific operations of power-on check, time measurement function, current function, aviation function, exit menu, menu switching, brightness adjustment and reset.
Further, the operation steps of the horological function include:
pressing a time measurement button, enabling the simulation aviation clock system to enter a time measurement function, and starting time measurement;
pressing the time measuring button again, and stopping time measurement;
and pressing the time measurement button for the third time, and resetting the time measurement to zero.
Further, the operation step of the current function comprises:
pressing a menu button, and enabling the simulation aviation clock system to enter a timing page;
pressing the menu button again, switching three options of second, minute and hour through a selection frame arranged in the display, and once the time measurement button is pressed, performing unidirectional accumulation on numbers in the selection frame by 1;
and after the current time is adjusted, simultaneously pressing the menu button and the time measurement button, and quitting the time correction page.
Further, the operation steps of the time-of-flight function include:
pressing the menu button twice, reading the option of the total time of flight through the inside of the display in the selected frame, and then pressing the time measuring button to read the accumulated value of the aircraft time of flight;
and pressing the menu button again, and pressing the time measuring button through the option of deleting the log in the display in the selected frame to clear the navigation time and the accumulated value of the airplane.
The invention has the beneficial effects that: the system function is realized by interacting software and upper computer data to control a hardware instrument, so that the structure of the simulation aviation clock is similar to a real aviation clock, the operation mode is consistent with that of a real aircraft aviation clock, and the difference is that the system working logic is completed by software simulation, so that the training and experience consistent with the flight driving of a real aircraft can be obtained only by simulating the driving of the aviation aircraft in the aviation flight simulator, the authenticity and the rigidness of the flight simulation process are further improved, the learning capacity of a pilot is improved, and the training requirements of the pilot are met. Meanwhile, the simulated aviation clock can simultaneously display and record the current standard time, the aviation flight time and the timing time, so that the problems of limitation and deficiency of the aviation clock in the prior art are solved, and the simulated aviation clock is simple to operate and accurate in timing.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings needed in the embodiments will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art to obtain other drawings without creative efforts.
FIG. 1 is a system associated block diagram of a simulated aircraft clock system developed for a flight simulator in accordance with an embodiment of the invention;
FIG. 2 is a system flow diagram of a simulated aircraft clock system developed for a flight simulator in accordance with an embodiment of the invention;
FIG. 3 is a connection topology diagram of a cockpit operations human-machine interface in a simulated airborne clock system developed for a flight simulator in accordance with an embodiment of the present invention;
FIG. 4 is a workflow diagram of a method of operation of a simulated aircraft clock system developed for a flight simulator in accordance with an embodiment of the invention;
FIG. 5 is a diagram of mode responder energy supply in a method of operation of a simulated aircraft clock system developed for a flight simulator, according to an embodiment of the invention;
FIG. 6 is a page view of reading and deleting an aircraft clock time-of-flight cumulative value in a method of operation of a simulated aircraft clock system developed for a flight simulator, according to an embodiment of the invention.
Detailed Description
For further explanation of the various embodiments, the drawings which form a part of the disclosure and which are incorporated in and constitute a part of this specification, illustrate embodiments and, together with the description, serve to explain the principles of operation of the embodiments, and to enable others of ordinary skill in the art to understand the various embodiments and advantages of the invention, and, by reference to these figures, reference is made to the accompanying drawings, which are not to scale and wherein like reference numerals generally refer to like elements.
According to an embodiment of the present invention, a simulated aircraft clock system developed for a flight simulator and a method of operating the same are provided.
The present invention will now be further described with reference to the accompanying drawings and detailed description, wherein as shown in fig. 1-3, a simulated aircraft clock system developed for a flight simulator according to an embodiment of the present invention comprises:
the power-on module is used for realizing voltage conversion and carrying out power-on inspection on the interior of the system;
the fault analysis response module is used for capturing the fault state of the system and analyzing to realize corresponding response;
the brightness adjusting module is used for adjusting the brightness of the simulation display in the system hardware instrument;
the current calculating module is used for calculating current time;
the time measurement calculating module is used for realizing a timing function;
the time of flight resolving module is used for calculating the time of flight and calculating the accumulated value of the time of flight;
and the reset resolving module is used for realizing reset and reset of the system.
In one embodiment, the simulated aircraft clock system is electrically connected to a cockpit simulation system (cockpit simulation computer), an electromechanical system, a flight system (aircraft performance simulation computer), an instructor station system (instructor console computer), and a cockpit simulation subsystem, in that order.
In one embodiment, the cabin simulation system provides onboard personnel operating information and lighting to the simulated airline clock system, which provides the current time, timing, and flight time to the cabin simulation subsystem.
In one embodiment, the electromechanical system provides a power supply signal for the simulated aircraft clock system.
In one embodiment, the flight system provides a landing gear lift off signal for the simulated aeronautical clock system.
In one embodiment, the instructor station system provides simulated fault information for the simulated aircraft clock system.
According to another embodiment of the present invention, as shown in fig. 4 to 6, there is also provided an operation method of a simulated aircraft clock system developed for a flight simulator, for implementing the operation of the simulated aircraft clock system, where a hardware instrument of the simulated aircraft clock system is provided with a brightness button, a reset button, a menu button, a time measurement button and a display, and is used for implementing specific operations of power-on check, time measurement function, current function, aircraft time function, exit menu, menu switching, brightness adjustment and reset.
The hardware instrument of the simulated aviation clock system adopts a simulated display, and the simulated display comprises a liquid crystal screen, a liquid crystal display screen driving circuit, a backlight component (a backlight luminous source, an optical component and the like), a controller (components such as brightness control, video signal conversion, power supply conversion, a serial interface, a video interface and the like) and the like. The display light guide plate key is collected and sent to the host computer by the CAN collection board, and the system function is realized through software and host computer data interaction and then control hardware instrument.
In addition, the aircraft is provided with three pieces of aircraft clocks which are respectively arranged on an instrument panel, a right instrument panel and a central control console and are used for displaying the current time, the navigation time and the timing time in flight for the pilot to view. The components of the aviation clock system which need to be powered include an aviation clock control box (right instrument panel), an aviation clock control box (central console) and an aviation clock control box (instrument panel), and the components are mainly powered by a 28V direct-current power supply. The aircraft clock retains visible hardware components within the cockpit, the hardware composition is shown in table 1 below, and the main component parameters are shown in table 2 below:
TABLE 1 aircraft clock hardware device List
TABLE 2 aviation clock parameter table
The operation steps of the power-on check comprise: and switching on an 'aircraft clock' self-protection switch on the breaker box, respectively observing that the current time windows on three main pages of the aircraft clock on the right instrument board, the central console and the instrument board have corresponding real-time display, and simultaneously, displaying a prompt symbol on the upper left of the screen and 2 prompt symbols on the upper right of the battery electric quantity.
In one embodiment, the operation of the horological function comprises:
pressing a time measurement button, enabling the simulation aviation clock system to enter a time measurement function, and starting time measurement;
pressing the time measuring button again, and stopping time measurement;
and pressing the time measurement button for the third time, and resetting the time measurement to zero.
In one embodiment, the operation of the nonce function comprises:
pressing a menu button, and enabling the simulation aviation clock system to enter a timing page;
pressing the menu button again, switching three options of second, minute and hour through a selection frame arranged in the display, and once the time measurement button is pressed, performing unidirectional accumulation on numbers in the selection frame by 1;
and after the current time is adjusted, simultaneously pressing the menu button and the time measurement button, and quitting the time correction page.
In one embodiment, the operating step of the time-of-flight function includes:
pressing the menu button twice, reading the option of the total time of flight through the inside of the display in the selected frame, and then pressing the time measuring button to read the accumulated value of the aircraft time of flight;
and pressing the menu button again, and pressing the time measuring button through the option of deleting the log in the display in the selected frame to clear the navigation time and the accumulated value of the airplane.
Wherein, pressing undercarriage interlocking terminal switch on the left main undercarriage, the time of flight on three aviation clocks should be from "00: 00: 00', starting timing, loosening the left main undercarriage interlocking terminal switch, and stopping changing the flight time number; the interlocking terminal switch of the left main landing gear is pressed again within 10S, and the display number is accumulated on the number of flight hours before stopping; the aviation clock automatically accumulates the current time and the historical time; if the left main landing gear interlocking terminal switch is pressed again after 10S, the flight time number on the three aviation clocks is from' 00: 00: 00' start timing, the above is the initial calculation operation step of the time of flight in single flight.
In addition, the operation step of exiting the menu includes: and when the time measurement button is pressed, page turning is carried out, the aviation clock enters the aviation clock exit page, the menu button is pressed, and the aviation clock returns to the main page.
The operation steps of menu switching comprise: pressing a menu button on a hardware instrument of the aviation clock on a main page of the aviation clock, entering a timing page of the aviation clock, and performing downward shifting switching on the function of the screen through a timing button; pressing the menu button again to enter the next functional page; and when the function setting page is displayed, the menu button and the time measuring button are pressed simultaneously, and the aviation clock main page is returned.
The operation steps of brightness adjustment include: and when the brightness button on the aviation clock hardware instrument is pressed, the brightness of the aviation clock display screen is changed, the brightness is adjustable at 5 levels, the brightness of the screen is increased by one level every time, the brightness button is pressed again when the brightness reaches the brightest, the brightness is changed into the lowest brightness, and the cycle is repeated.
The reset operation comprises the following steps: when the aviation clock is in an abnormal time-lapse condition, a reset button is pressed on the main page, and then the system reset is completed. After the aviation clock is restarted, the screen displays the current time, and the aviation clock and the time measuring clock stop after being reset. And simultaneously, 2 prompt symbols of the battery electric quantity appear at the upper left and the upper right of the screen respectively and disappear after 3 s.
In addition, the fault analysis process and the specific operation method in the simulation aeronautical clock system are as follows:
(1) aeronautical clock 1 fault (Right dashboard)
a) Trigger logic
The instructor station operator selects "aeronautical clock 1 fault" in the fault simulation unit. And (3) capturing the fault state by the system, and stopping all the work flows of the aviation clock 1 in the software.
b) Response logic
1) The left instrument board aviation clock stops timing at present;
2) stopping timing by the left instrument board aviation clock during the aviation;
3) the left instrument board aviation clock time measurement stops timing;
4) the reset knob switch of the aviation clock of the left instrument board is invalid;
5) the left instrument board aviation clock menu button switch is invalid;
6) the button switch is invalid when the left instrument board aviation clock is measured;
c) associative logic
Is free of
(2) Aeronautical clock 2 fault (center console)
a) Trigger logic
The instructor station operator selects "aeronautical clock 2 failure" in the failure simulation unit. The system captures the fault state and all the work flows of the aviation clock 2 in the software are stopped.
b) Response logic
1) The central control console aviation clock stops timing at present;
2) stopping timing when the central control console is used for aeronautical clock;
3) the time measurement of the aviation clock of the central control console stops timing;
4) the reset button switch of the aviation clock of the central control console is invalid;
5) the button switch of the aviation clock menu of the central control console is invalid;
6) the button switch is invalid when the aviation clock of the central control console measures time;
c) associative logic
None.
(3) Aviation clock 3 fault (Instrument board)
a) Trigger logic
The instructor station operator selects "aeronautical clock 3 fault" in the fault simulation unit. The system captures the fault state and all the work flows of the aviation clock 3 in the software are stopped.
b) Response logic
1) The aviation clock stops timing at present;
2) stopping timing by an aviation clock during aviation;
3) stopping timing when the aviation clock measures time;
4) the reset button switch of the aviation clock fails;
5) the aviation clock menu button switch is invalid;
6) the button switch is invalid when the aviation clock is measured;
c) associative logic
Is free of
In addition, the input interface of the interface control ICD of the aircraft clock system is described in table 3 below, and the output interface is described in table 4 below:
TABLE 3 aviation clock input interface table
TABLE 4 output interface table of aviation clock
In summary, according to the technical scheme of the invention, the system function is realized by software and upper computer data interaction to control a hardware instrument, so that the structure of the simulation aircraft clock in the invention is similar to a real aircraft clock, and the operation mode is consistent with that of a real aircraft clock. Meanwhile, the simulated aviation clock can simultaneously display and record the current standard time, the aviation flight time and the timing time, so that the problems of limitation and deficiency of the aviation clock in the prior art are solved, and the simulated aviation clock is simple to operate and accurate in timing.
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 simulated aircraft clock system developed for a flight simulator, the simulated aircraft clock system comprising:
the power-on module is used for realizing voltage conversion and carrying out power-on inspection on the interior of the system;
the fault analysis response module is used for capturing the fault state of the system and analyzing to realize corresponding response;
the brightness adjusting module is used for adjusting the brightness of the simulation display in the system hardware instrument;
the current calculating module is used for calculating current time;
the time measurement calculating module is used for realizing a timing function;
the time of flight resolving module is used for calculating the time of flight and calculating the accumulated value of the time of flight;
and the reset resolving module is used for realizing reset and reset of the system.
2. The simulated aerial clock system developed for a flight simulator of claim 1, wherein the simulated aerial clock system is electrically connected to a cockpit simulation system, an electromechanical system, a flight system, an instructor's station system, and a cockpit simulation subsystem, in that order.
3. The simulated aerial clock system developed for a flight simulator of claim 2, wherein the cabin simulation system provides onboard personnel operational information and lighting for the simulated aerial clock system, the simulated aerial clock system providing time of day, timing and time of flight for the cabin simulation subsystem.
4. The simulated aeronautical clock system developed for flight simulator of claim 2, wherein the electromechanical system provides a power supply signal to the simulated aeronautical clock system.
5. The simulated aeronautical clock system developed for flight simulator and method of operation thereof of claim 2, wherein the flight system provides a landing gear off ground signal for the simulated aeronautical clock system.
6. The simulated aircraft clock system developed for a flight simulator and method of operation thereof as claimed in claim 2 wherein the instructor's station system provides simulated fault information for the simulated aircraft clock system.
7. An operation method of a simulated aviation clock system developed aiming at a flight simulator is used for realizing the operation of the aviation clock system in the claim 1, and is characterized in that a hardware instrument of the simulated aviation clock system is provided with a brightness button, a reset button, a menu button, a time measurement button and a display and is used for realizing the specific operations of power-on inspection, time measurement function, current function, aviation function, exit menu, menu switching, brightness adjustment and reset.
8. The method of operating a simulated airborne clock system developed for a flight simulator of claim 7, wherein the step of operating the horological function comprises:
pressing a time measurement button, enabling the simulation aviation clock system to enter a time measurement function, and starting time measurement;
pressing the time measuring button again, and stopping time measurement;
and pressing the time measurement button for the third time, and resetting the time measurement to zero.
9. The method of operating a simulated aircraft clock system developed for a flight simulator of claim 8, wherein the step of operating the current function comprises:
pressing a menu button, and enabling the simulation aviation clock system to enter a timing page;
pressing the menu button again, switching three options of second, minute and hour through a selection frame arranged in the display, and once the time measurement button is pressed, performing unidirectional accumulation on numbers in the selection frame by 1;
and after the current time is adjusted, simultaneously pressing the menu button and the time measurement button, and quitting the time correction page.
10. The method of operating a simulated airborne clock system developed for a flight simulator of claim 9, wherein the step of operating the time-of-flight function comprises:
pressing the menu button twice, reading the option of the total time of flight through the inside of the display in the selected frame, and then pressing the time measuring button to read the accumulated value of the aircraft time of flight;
and pressing the menu button again, and pressing the time measuring button through the option of deleting the log in the display in the selected frame to clear the navigation time and the accumulated value of the airplane.
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Cited By (1)
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Application publication date: 20210507 |