CN114153510A - Method for customizing head-up display picture - Google Patents
Method for customizing head-up display picture Download PDFInfo
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- CN114153510A CN114153510A CN202111553845.XA CN202111553845A CN114153510A CN 114153510 A CN114153510 A CN 114153510A CN 202111553845 A CN202111553845 A CN 202111553845A CN 114153510 A CN114153510 A CN 114153510A
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- 238000000034 method Methods 0.000 title claims abstract description 14
- 230000003631 expected effect Effects 0.000 abstract description 2
- 230000000007 visual effect Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
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- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F9/00—Arrangements for program control, e.g. control units
- G06F9/06—Arrangements for program control, e.g. control units using stored programs, i.e. using an internal store of processing equipment to receive or retain programs
- G06F9/46—Multiprogramming arrangements
- G06F9/54—Interprogram communication
- G06F9/541—Interprogram communication via adapters, e.g. between incompatible applications
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- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F9/00—Arrangements for program control, e.g. control units
- G06F9/06—Arrangements for program control, e.g. control units using stored programs, i.e. using an internal store of processing equipment to receive or retain programs
- G06F9/44—Arrangements for executing specific programs
- G06F9/4401—Bootstrapping
- G06F9/4411—Configuring for operating with peripheral devices; Loading of device drivers
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- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F9/00—Arrangements for program control, e.g. control units
- G06F9/06—Arrangements for program control, e.g. control units using stored programs, i.e. using an internal store of processing equipment to receive or retain programs
- G06F9/44—Arrangements for executing specific programs
- G06F9/451—Execution arrangements for user interfaces
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Abstract
The invention relates to a method for customizing characters of a display picture of a head-up display, and belongs to the field of design of airplane avionics systems. A method for customizing a highlight picture comprises the following steps: firstly, a pilot edits in a ground mission planning station according to own requirements and habits to determine characters needing to be displayed in a head-up display mode; step two, after editing is finished, generating a head-up display demonstration picture, numbering and storing the head-up display demonstration picture, and storing the head-up display demonstration picture in a ground mission planning station; and thirdly, loading data in the ground mission planning station into a data card through an adapter, inserting the data card into a data loading recorder, loading the data onto the aircraft head display through the data card after the system is powered on, and displaying the data on the head display according to different modes of the avionic system according to the data loaded by the pilot. The invention has the following advantages: the head up display software is not required to be upgraded and improved, the head up display picture is self-defined and flexibly set, the requirements of different pilots are met, manpower and material resources are saved, and the expected effect is achieved.
Description
Technical Field
The invention relates to a method for customizing characters of a display picture of a head-up display, and belongs to the technical field of design of airplane avionics systems.
Background
The head-up display is arranged on an instrument board of an aircraft cockpit and positioned right in front of a pilot, provides flight data such as navigation data and weapon attack data for the pilot, and implements congestion prevention display on the head-up display in order to make a head-up display picture concise and clear, reduce the visual burden of the pilot at present. The head-up display picture is divided into three modes of 'normal', 'anti-congestion 1' and 'anti-congestion 2'. The "normal" mode: displaying a complete flat display picture; "anti-congestion 1" mode: the characters such as the scrolling scale band on the head-up display and the data blocks at the upper left corner and the upper right corner are not displayed, and the 'anti-congestion 2' mode: except the content of 'anti-congestion 1' on the HUD, characters such as a heading scale band, a speed scale band and a height scale band are not displayed.
The existing airplane head-up display method has the following problems: the current display content is fixed, the character content displayed in each mode is determined by software, a pilot cannot perform self-defined display on a head-up display picture according to own requirements, if the pilot disagrees with the displayed picture, the head-up display software needs to be upgraded again, but the requirements of different pilots on display are different, so that the head-up display software is continuously upgraded to meet the requirements of different pilots.
Disclosure of Invention
The invention aims to provide a method for customizing a head-up display picture, so that different pilots can customize the display picture according to own habits and requirements.
In order to achieve the purpose, the invention adopts the following technical scheme: a method for customizing a highlight picture comprises the following steps:
firstly, a pilot edits in a ground mission planning station according to own requirements and habits to determine characters needing to be displayed in a head-up display mode;
step two, after editing is finished, generating a head-up display demonstration picture, numbering and storing the head-up display demonstration picture, and storing the head-up display demonstration picture in a ground mission planning station;
and thirdly, loading data in the ground mission planning station into a data card through an adapter, inserting the data card into a data loading recorder, loading the data onto the aircraft head display through the data card after the system is powered on, and displaying the data on the head display according to different modes of the avionic system according to the data loaded by the pilot.
Preferably, the modes of the avionics system comprise an air-space mode, an air-ground mode, a navigation mode and an approach landing mode, and the display is performed according to the four modes.
Preferably, three sub-modes of "normal", "anti-congestion 1" and "anti-congestion 2" are set in each of the four modes.
Preferably, in step three, the head-up display stores the loaded parameter data in the nonvolatile memory, and the parameter data is not influenced by the power-on and power-off of the head-up display.
Preferably, after the flat display is powered on, the stored data is used by default, whether new loading data is received or not is judged, and if the new loading data is received, the data is stored into the nonvolatile memory to cover the data stored last time; otherwise, the stored data is used.
Compared with the prior art, the invention has the following advantages: the head-up display software does not need to be upgraded and improved, the head-up display picture is self-defined and flexibly set, the requirements of different pilots are met, manpower and material resources are saved, and the expected effect is achieved.
Drawings
FIG. 1 is a schematic diagram of a flat-screen display according to an embodiment of the present invention;
1. displaying the picture; 2. and a parameter display area.
Detailed Description
The invention is described in further detail below: a method for customizing a highlight picture comprises the following steps:
firstly, a pilot edits in a ground mission planning station according to own requirements and habits to determine characters needing to be displayed in a flat display mode, namely which characters need to be displayed and which characters do not need to be displayed;
step two, after editing is finished, a head-up display demonstration picture is generated, and after the pilot confirms that the display is correct, the pilot numbers and stores the head-up display demonstration picture in a ground mission planning station;
and thirdly, loading data in the ground mission planning station into a data card through an adapter, inserting the data card into a data loading recorder, loading the data onto the aircraft head display through the data card after the system is powered on, and displaying the data on the head display according to different modes of the avionic system according to the data loaded by the pilot.
Because the field of view of the head-up display is limited, all flight parameters cannot be displayed like a down-view display, and therefore, the flight parameters need to be selectively displayed according to flight missions in different modes. According to different flight missions, the modes of the avionic system are respectively an air-space mode, an air-ground mode, a navigation mode and an approach landing mode. In order to make the head-up display picture concise and clear and reduce the visual burden of pilots, the head-up display picture is displayed in an anti-congestion way. And three sub-modes of 'normal', 'anti-congestion 1' and 'anti-congestion 2' are set in each mode. In order to realize the self-definition of the head-up display picture 1, a pilot carries out self-definition in the ground mission planning station according to the requirements of each mode, names the pilot with the pilot number after editing is finished, and stores the pilot number into the ground mission planning station. In the next flight, the pilot can directly load the aircraft display without repeated planning when the parameters are not required to be modified.
If in the navigation mode, the parameter display area 2 mainly focuses on displaying navigation parameters, such as flight speed, altitude, course, waypoint, arrival point, distance to be flown, yaw distance and other information, and for a primary pilot, displaying more comprehensive navigation parameters; for middle or high pilot, a simple picture is displayed, such as speed, height scale band and the like are not displayed. In addition, every pilot hobby is different, and some pilots set up and instruct airspeed, the vacuum speed to show simultaneously, and some pilots set up and instruct airspeed, the ground speed to show simultaneously.
Setting is carried out under a head-up display picture setting interface of the ground mission planning station, all parameters are displayed under the default condition, each parameter can be selected or not selected, a pilot selects according to self requirements and different modes, a head-up display demonstration picture is generated after selection is completed, and the pilot verifies whether the displayed picture is correct or not. And after the completion, naming and storing the pilot number, and storing the pilot number into a ground mission planning station. Data in a planning station is loaded into a data card through an adapter, the data card is inserted into a data loading recorder, after the system is powered on, head-up display parameter data in the data card is loaded into a head-up display, and the head-up display carries out corresponding display according to four modes of an air-space mode, an air-ground mode, a navigation mode and an approach landing mode of an aviation system and three sub-modes of 'normal', 'anti-jamming 1' and 'anti-jamming 2'. Meeting the requirements of pilots.
The head-up display stores the loaded parameter data in the nonvolatile memory, and is not influenced by the power-on and power-off of the head-up display, so that the head-up display does not need to be repeatedly loaded when the same pilot flies the same airplane;
the ground mission planning station stores the head-up parameter data loaded by the pilots, so that after each pilot edits the data once, if the requirements do not change, the data can be loaded to airplanes with different shelves without repeated editing.
The head-up display logic is as follows:
in the task preparation phase: after the head up display is powered on, the stored data is used by default, whether new loading data is received or not is judged, if yes, the data is stored into the nonvolatile memory, and the data stored last time is overwritten; otherwise, the stored data is used.
After the avionics system works normally, the flat display carries out picture display according to four main modes and three sub-modes issued by the avionics system and the stored corresponding modes.
Claims (5)
1. A method for customizing a highlight picture comprises the following steps:
firstly, a pilot edits in a ground mission planning station according to own requirements and habits to determine characters needing to be displayed in a head-up display mode;
step two, after editing is finished, generating a head-up display demonstration picture, numbering and storing the head-up display demonstration picture, and storing the head-up display demonstration picture in a ground mission planning station;
and thirdly, loading data in the ground mission planning station into a data card through an adapter, inserting the data card into a data loading recorder, loading the data onto the aircraft head display through the data card after the system is powered on, and displaying the data on the head display according to different modes of the avionic system according to the data loaded by the pilot.
2. The method for customizing a highlight picture according to claim 1, wherein: the modes of the avionic system comprise an air-space mode, an air-ground mode, a navigation mode and an approach landing mode, and the display is performed according to the four modes.
3. The highlight picture customization method according to claim 2, wherein: and setting three sub-modes of 'normal', 'anti-congestion 1' and 'anti-congestion 2' in each of the four modes.
4. The method for customizing a highlight picture according to claim 1, wherein: in the third step, the head-up display stores the loaded parameter data in the nonvolatile memory, and the head-up display is not influenced by the power-on and power-off of the head-up display.
5. The method for customizing a highlight picture according to claim 1, wherein: after the head up display is powered on, the stored data is used by default, whether new loading data is received or not is judged, if yes, the data is stored into the nonvolatile memory, and the data stored last time is overwritten; otherwise, the stored data is used.
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Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103513922A (en) * | 2012-06-25 | 2014-01-15 | 霍尼韦尔国际公司 | Avionics display system providing enhanced flight-plan management |
CN104299068A (en) * | 2014-08-27 | 2015-01-21 | 南京航空航天大学 | Cabin display control information management system and method based on ARINC 661 |
CN104859862A (en) * | 2014-02-26 | 2015-08-26 | 霍尼韦尔国际公司 | Pilot Centered System And Method For Decluttering Aircraft Displays |
CN105335158A (en) * | 2015-10-29 | 2016-02-17 | 西安电子科技大学 | Flight interface display method based on ARINC661 custom symbol library |
CN107024978A (en) * | 2015-07-31 | 2017-08-08 | 泰勒斯公司 | Manage the man-machine interface of aircraft flight |
CN108037970A (en) * | 2017-12-07 | 2018-05-15 | 中国航空无线电电子研究所 | Build the instrument and its method of civil aircraft cockpit man-machine interface rapid prototyping |
CN108557091A (en) * | 2018-04-13 | 2018-09-21 | 成都赫尔墨斯科技股份有限公司 | A kind of device and method for integrating head-up display in Aerial Electronic Equipment |
CN110083318A (en) * | 2019-03-20 | 2019-08-02 | 中国航空无线电电子研究所 | A kind of high-performance cockpit display system that more CDS examples are integrated |
CN110531978A (en) * | 2019-07-11 | 2019-12-03 | 北京机电工程研究所 | A kind of cockpit display system |
CN112184950A (en) * | 2020-10-10 | 2021-01-05 | 江西洪都航空工业集团有限责任公司 | Four-card-in-one data loading recording method |
-
2021
- 2021-12-17 CN CN202111553845.XA patent/CN114153510A/en active Pending
Patent Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103513922A (en) * | 2012-06-25 | 2014-01-15 | 霍尼韦尔国际公司 | Avionics display system providing enhanced flight-plan management |
CN104859862A (en) * | 2014-02-26 | 2015-08-26 | 霍尼韦尔国际公司 | Pilot Centered System And Method For Decluttering Aircraft Displays |
CN104299068A (en) * | 2014-08-27 | 2015-01-21 | 南京航空航天大学 | Cabin display control information management system and method based on ARINC 661 |
CN107024978A (en) * | 2015-07-31 | 2017-08-08 | 泰勒斯公司 | Manage the man-machine interface of aircraft flight |
CN105335158A (en) * | 2015-10-29 | 2016-02-17 | 西安电子科技大学 | Flight interface display method based on ARINC661 custom symbol library |
CN108037970A (en) * | 2017-12-07 | 2018-05-15 | 中国航空无线电电子研究所 | Build the instrument and its method of civil aircraft cockpit man-machine interface rapid prototyping |
CN108557091A (en) * | 2018-04-13 | 2018-09-21 | 成都赫尔墨斯科技股份有限公司 | A kind of device and method for integrating head-up display in Aerial Electronic Equipment |
CN110083318A (en) * | 2019-03-20 | 2019-08-02 | 中国航空无线电电子研究所 | A kind of high-performance cockpit display system that more CDS examples are integrated |
CN110531978A (en) * | 2019-07-11 | 2019-12-03 | 北京机电工程研究所 | A kind of cockpit display system |
CN112184950A (en) * | 2020-10-10 | 2021-01-05 | 江西洪都航空工业集团有限责任公司 | Four-card-in-one data loading recording method |
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