The present invention relates to an electronic display device for a glass cockpit of a vehicle control system, said cockpit comprising a plurality of screens, at least two screens of the plurality of screens being able to simultaneously display separate video streams respectively associated with different display formats.
The invention also relates to a vehicle, such as an aircraft, comprising a glass cockpit and further comprising such a display device.
The invention also relates to a display method for a glass cockpit of a vehicle implemented by such a display device of the vehicle.
The invention also relates to a computer program product including software instructions which, when implemented by computer equipment, carry out such a display method.
A vehicle refers to any apparatus able to move between two different geographical positions. Such a vehicle for example corresponds to an aircraft.
An aircraft refers to any piloted vehicle capable of flying at least within the Earth's atmosphere, such as an airplane or a helicopter.
A format refers to a screen region dedicated to displaying a set of elements associated with a predetermined function of the control system. For example, the format dedicated to displaying primary flight parameters (PFD, Primary Flight Display) corresponds to a screen region containing all of the elements allowing the pilot to control and/or pilot his vehicle, namely the attitude, speed, altitude, etc.
The present invention relates to the field of a display for a glass cockpit, in particular in an aircraft cockpit, also called CDS (Cockpit Display System) or in any other vehicle comprising a cockpit area with reconfigurable display elements.
The new generations of cockpit solutions are equipped with glass cockpits, in which the conventional dedicated hardware equipment items, such as needle instruments, are “virtualized” (that is to say, replaced) by screens, in particular LCD screens, together forming a coherent viewing surface. In other words, the set of screens provides display and interaction coherence between screens, a pilot being able to point with the cursor of his control member on the various screens.
Such an equipment virtualization results in increasing the number of displayable formats, the screens making it possible to display essential information for the control of the vehicle, such as that relative to navigation, communications provided by the embedded systems obeying certain integrity and availability constraints such as avionics systems when the vehicle is an aircraft.
The screens also make it possible to provide information other than that which is essential for the control of the vehicle, such as navigation maps, virtualized control panels, external camera video streams, control manuals, etc.
The number of displayable formats generally greatly exceeds the total display surface proposed by the screens of the glass cockpit, such that the pilot must reconfigure the display of the cockpit based on his operational needs or the mission assigned to the vehicle.
Such a task is complex to perform mentally in an optimal manner, since the number of possible display combinations is multiplied by the number of formats, the number of screens, and the number of display configurations within a same screen, and creates insecurity in particular if the pilot inadvertently deletes information that is essential for the control of the vehicle.
The aim of the invention is to propose a user (that is to say, pilot) entry mechanism for configuring the display of a glass cockpit, allowing the user to directly define different processing conditions of the display while keeping an optimal useful information retrieval area.
To that end, the invention relates to an electronic display device for a glass cockpit of a vehicle control system, said cockpit comprising a plurality of screens, at least two screens of the plurality of screens being able to simultaneously display separate video streams respectively associated with different display formats, the display device comprising, for each screen of at least part of the plurality of screens, an interactive display configuration tool, the device being configured, for each screen of said at least part, to:
display the configuration tool in at least one predetermined zone of said screen, the configuration tool comprising a plurality of user entry symbols, each symbol being associated with a display configuration corresponding to the combination of a display format, a display window size of said display format relative to the size of said screen, and a location of said display window of the display format within said screen,
modify the display configuration of said screen if a user entry symbol is selected that is different from the user entry symbol corresponding to the current display configuration of said screen.
Thus, with the electronic display device according to the invention, the user entry mechanism makes it possible, through the selection of a single user entry symbol, to directly apply a display configuration corresponding to a triplet of simultaneous settings, namely a setting pertaining to the display format, a setting pertaining to the display window size of the display format relative to the size of the considered screen, and the setting of a location of the display window of the display format within the screen, able to retrieve, if applicable, a combination of formats.
The display device according to the invention is then particularly advantageous to configure or reconfigure, locally, the display of each screen of a glass cockpit, in particular in case of new mission of the vehicle or navigation phase (e.g., departure or takeoff for an aircraft, cruising, arrival or landing for an aircraft, etc.).
Indeed, the display device according to the present invention concretely helps the user perform a local reconfiguration of the display of a glass cockpit using a man-machine interaction process guided by the selection of user entry symbol(s) within the configuration tool locally associated with each screen, each entry symbol being explicitly representative, for any user, of the display configuration (that is to say, a triplet of simultaneous settings of the display of the considered screen) that is associated therewith.
There is therefore a reliable causal link between the assistance provided to any user and the display device, in particular the signaling done, by the display device, using configuration tools each associated with a screen of the glass cockpit and each comprising the user entry symbols proposed above.
According to other advantageous aspects of the invention, the electronic display device comprises one or more of the following features, considered alone or according to all technically possible combinations:
the display device is configured to display the interactive display configuration tool continuously and/or temporarily on the video stream(s) being displayed on said screen, and wherein:
in order to display the configuration tool temporarily, the display device can be activated by:
when the interactive display configuration tool is configured to be displayed temporarily, the device is configured to close the configuration tool automatically after activation of the user entry symbol, and/or after expiration of a predetermined time period, and/or after detection of a user entry outside of said at least one predetermined display zone of the configuration tool;
the display device is configured to make a user entry symbol selectable from said plurality of user entry symbols as a function of the current display configuration of said screen and/or as a function of the position of said screen within said cockpit and/or as a function of the current display configuration of at least one other screen of said plurality of screens, said at least one other screen being separate from said screen;
the configuration tool corresponds to a sequenced list of the set of display configurations of the formats displayable on at least one of the screens of said plurality of screens, each row of the sequenced list being associated with the display format of said set of displayable display formats and comprising as many user entry symbols as there are display configuration(s) associated with said display format of the row and displayable at least once on said screen;
when the interactive display configuration tool is configured to be displayed temporarily, the order of the set of display configurations of the displayable display formats of the sequenced list is invariable from one screen of the plurality of screens to the next;
the display device is configured to display each user entry symbol according to four distinct states corresponding to:
the current display configuration,
a display configuration displayable from the current display configuration,
a display configuration displayable at least once on said screen but not displayable from the current display configuration,
a display configuration never displayable on said screen.
The invention also relates to a vehicle, such as an aircraft, comprising a glass cockpit, the vehicle further comprising a display device as defined above.
The invention also relates to a display method for a glass cockpit of a vehicle implemented by a display device of the vehicle, the device being intended to provide video streams to a plurality of viewing screens of said cockpit, at least two screens of the plurality of screens being able to simultaneously display separate video streams respectively associated with separate display formats, the device comprising an interactive display configuration tool, for each screen of said at least one part, the method comprising at least:
displaying the configuration tool in at least one predetermined zone of said screen, the configuration tool comprising a plurality of user entry symbols, each symbol being associated with a display configuration corresponding to the combination of a display format, a display window size of said display format relative to the size of said screen, and a location of said display window of the display format within said screen,
modifying the display configuration of said screen if a user entry symbol is selected that is different from the user entry symbol corresponding to the current display configuration of said screen.
The invention also relates to a computer program including software instructions which, when executed by a computer, implement a display method as defined above.
These features and advantages of the invention will appear more clearly upon reading the following description, provided solely as a non-limiting example, and done in reference to the appended drawings, in which:
In the remainder of the description, the expression “substantially equal to” designates a relationship of equality to within plus or minus 10%, preferably to within plus or minus 5%.
In
According to the example of
The combination of the N processing units U1, U2, U3, . . . , UN forms the display device according to the present invention configured to locally adapt the display of a screen, independently from one screen to another.
According to one aspect that is not shown, only P screens among the N are associated with a processing unit allowing the reconfiguration of their own display, P being strictly less than N, the format of the N-P other screens of the glass cockpit not being reconfigurable and as a result being permanent, in particular for safety reasons.
According to the present invention, the display device comprises, respectively for each screen of (all or part of) the plurality of screens E1, E2, E3, . . . , EN, an interactive display configuration tool O1, O2, O3, . . . , ON.
According to one particular aspect, the display device is able to be activated, irrespective of the flight conditions, by manual action by the user, for example by: mechanical pressure on a dedicated and/or existing physical button (or cursor) of each screen of the plurality of screens of the glass cockpit; and/or by tactile pressure or pointing on a virtual button of each screen, and/or by a predetermined tactile gesture on the surface of each screen.
A predetermined tactile gesture for example refers to a double or triple tap by a finger, a continuous finger swipe, a separation of two fingers on the tactile surface of the screen, etc.
In the example of
Likewise, the interactive display configuration tool O2 is made in the form of software, or a software component executable by the processor P2 of the processing unit U2 associated with the screen E2. The memory M2 is then able to store such interactive display software O2 to locally allow the configuration of the display of the screen E2. The processor P2 is then able to execute such interactive display software O2.
The interactive display configuration tool O3 is also made in the form of software, or a software component executable by the processor P3 of the processing unit U3 associated with the screen E3. The memory M3 is then able to store such interactive display software O3 to locally allow the configuration of the display of the screen E3. The processor P3 is then able to execute such interactive display software O3.
And so forth until the interactive display configuration tool ON is also made in the form of software, or a software component executable by the processor PN of the processing unit UN associated with the screen EN. The memory MN is then able to store such interactive display software ON to locally allow the configuration of the display of the screen EN The processor PN is then able to execute such interactive display software ON.
In a variant, the interactive display configuration tools O1, O2, O3, . . . , ON are each made in the form of a programmable logic component, such as an FPGA (Field Programmable Gate Array), or in the form of a dedicated integrated circuit, such as an ASIC (Application Specific Integrated Circuit).
When part of the display device is made in the form of one or several software programs, i.e., in the form of a computer program, this part is further able to be stored on a medium, not shown, readable by computer. The computer-readable medium is for example a medium suitable for storing electronic instructions and able to be coupled with a bus of a computer system. As an example, the readable medium is an optical disc, a magnetic-optical disc, a ROM memory, a RAM memory, any type of non-volatile memory (for example, EPROM, EEPROM, FLASH, NVRAM), a magnetic card or an optical card. A computer program including software instructions is then stored on the readable medium.
According to the example of
In the example of
According to one particular aspect, the configuration tool O1 corresponds to a sequenced list of the set of display configurations of the formats F1, F2, F3 . . . F10 displayable on at least one of the screens of the plurality of screens E1, E2, E3, . . . , EN.
As a non-limiting example, the first format F1 corresponds to the format dedicated to the display of primary flight parameters (PFD, Primary Flight Display), the format F2 is the format dedicated to the display of navigation parameters (ND, Navigation Display), such as the heading, the format F3 is dedicated to the display of parameters associated with the mission of the vehicle, such as the search and rescue mission, an oil and gas mission, etc., the format F4 is dedicated to the display of virtualized control panels for example allowing a three-dimensional representation of the relief, an aeronautic diagram or a depiction of an airport, the format F5 is dedicated to the flight management system (FMS), the format F6 is dedicated to the configuration of communication means, for example high frequency HF and very high frequency VHF, the format F7 is dedicated to the monitoring of the states of elements of the piloting system, the format F8 is dedicated to the display of piloting procedures, the format F9 is dedicated to the display of external camera video streams, the format F10 is dedicated to the display of map(s), etc.
Any other format wording combination F1, F2, F3 . . . F10 in the aforementioned examples of formats can be considered, for example the wording format F7 is dedicated to the display of map(s), while the wording format F10 is dedicated to monitoring the states of elements of the piloting system.
More specifically according to this particular aspect, each row of the sequenced list is associated with a display format of the set of displayable display formats and comprises as many user entry symbols as there are associated display configuration(s) associated with the display format of the row and displayable at least once on the considered screen.
In particular, the display device is configured to display each user entry symbol according to four different states corresponding to the current display configuration, a display configuration displayable from the current display configuration, a display configuration displayable at least once on said screen but not displayable from the current display configuration, a display configuration never displayable on said screen.
These four states are predetermined, known by the user and explicit (that is to say, each obviously associated for any user with a display configuration that is specific to it).
According to the example of
The absence of user entry symbol (that is to say, contour) indicates to the user that the associated display configuration is never displayable on the considered screen.
The filling of the contour of a user entry symbol by a texture, dots according to the example of
Thus, in particular considering the configuration tool O1 associated with the screen E1, the current display configuration is therefore shown by a user entry symbol in dotted lines and in particular corresponds to the display of the format F1 in the window E1W1 on the left of the screen E1 and the display of the format F3 in the window E1W2 of this same screen E1. The size of each of the windows E1W1 and E1W2 is equal to the size of the half-screen E1.
The format F1 can also be displayed in full-screen, the symbol central to the oval contour of the line F1 being selectable. Conversely, in the screen E1, the symbol allowing the selection of the display configuration corresponding to the combination of the format F1, the window size corresponding to a half-screen, and the location on the right of this window is missing from the configuration tool O1, making it impossible to perform such a selection of a display configuration corresponding to a triplet of simultaneous settings, namely a setting relative to the display format, a setting relative to the display window size of the display format relative to the size of the considered screen, and the setting of a location of the display window of the display format within the screen.
Regarding the format F2, like the format F4, three user entry symbols are selectable in order to modify the current display configuration, namely a display of the format F2 in the window E1W1 on the left side of the screen E1, a display of the format F2 in full screen, and a display of the format F2 in the window E1W2 on the right side of the screen E1.
As previously indicated, the display of the format F3 in the right window E1W2 of this same screen E1 corresponds to the current display configuration, the format F3 is never displayable in full screen according to the example of
No display configuration of the format F5 is displayable (that is to say, accessible) on the screen E1, since no user entry symbol shown in
Regarding the formats F6 to F10, two user entry symbols are selectable in order to modify the current display configuration, namely a display of one of these formats in the window E1W1 on the left side of the screen E1 and a display of the format F2 in the window E1W2 on the right side of the screen E1.
Similarly, the display device, via the unit U2, is able to display the configuration tool O2 in the predetermined zone Z2 of the screen E2.
For the screen E2, the current display configuration is, according to the example of
Regarding the formats F1, F3 and F5 to F10, two user entry symbols are selectable in order to modify the current display configuration, namely a display of one of these formats in a window on the left side of the screen E2 and a display of the [sic] of one of these formats in a window on the right side of the screen E2.
Regarding the format F4, three user entry symbols are selectable in order to modify the current display configuration, namely a display of the format F4 in a window on the left side of the screen E2, a display of the format F4 in full screen, and a display of the format F4 in a window on the right side of the screen E2.
Similarly, the display device, via the unit U3, is able to display the configuration tool O3 in a predetermined zone Z3 of the screen E3.
For the screen E3, the current display configuration is, according to the example of
On the screen E3, in full screen, only the display of the format F1 is possible. To modify the current display configuration, the user can only select one of the user entry symbols associated with one of the formats F2 to F4 or one of the formats F6 to F10 associated with a display configuration of this format in a window located on the left side and of smaller size than the size of the screen E3.
No display configuration of the format F5 is displayable (that is to say, accessible) on the screen E3, since no user entry symbol shown in
The display configuration of the format F1 in a right window of predetermined size on the screen E3 is possible, but not displayable from the current display configuration, the round user symbol associated with the display of the format F1 in a right window having a finer contour than the other selectable user symbols. In other words, the display configuration of the format F1 in a right window of predetermined size on the screen E3 cannot directly follow from the current display configuration.
It should be noted that in the right window of the screen E3 in light of the selectable user entry symbols of the configuration tool O3, only the format F1 is retrievable in the right window of this screen E3 either via a full-screen configuration or via a configuration with a window equal in size to a half-screen located on the right side.
Similarly, the display device, via the unit UN, is able to display the configuration tool ON in a predetermined zone ZN of the screen EN
For the screen EN, the current display configuration in particular corresponds to the display of the format F9 in the window ENW1 on the left side of the screen EN and the display of the format F6 in the window ENW2 of this same screen EN. The size of each of the windows ENW1 and ENW2 is equal to the size of the half-screen EN.
No display configuration of the format F1 is displayable (that is to say, accessible) on the screen EN, since no user entry symbol shown in
Regarding the format F2, like the format F4, three user entry symbols are selectable in order to modify the current display configuration, namely a display of the format F2 in the window ENW1 on the left side of the screen EN, a display of the format F2 in full screen, and a display of the format F2 in the window ENW2 on the right side of the screen E1.
Regarding the formats F3, F5, F7, F8 and F10, two user entry symbols are selectable in order to modify the current display configuration, namely a display of one of these formats in a window on the left side of the screen EN and a display of one of these formats in a window on the right side of the screen EN.
As previously indicated, the display of the format F6 in the right window ENW2 of this same screen EN corresponds to the current display configuration, the format F6 is never displayable in full screen according to the example of
Likewise, the display of the format F9 in the left window ENW1 of this same screen EN corresponds to the current display configuration, the format F9 is never displayable in full screen according to the example of
According to one particular aspect, normative or technical constraints may impose or prevent certain display configurations, the display device according to the invention is configured to make automatically (that is to say, without human intervention) selectable (and conversely, non-selectable), a user entry symbol from the plurality of user entry symbols of the configuration tool as a function of the current display configuration of the considered screen and/or as a function of the position of the screen within the cockpit GC and/or as a function of the current display configuration of at least one other screen of the plurality of screens.
In other words, in relation with
According to the example of
In particular, when the interactive display configuration tool is configured to be displayed temporarily, the order of the set of display configurations of the displayable display formats of the sequenced list is invariable from one screen of the plurality of screens to the next. In other words, each interactive configuration tool O1, O2, O3, . . . ON comprises a first line associated with the same format F1 from one configuration tool to the next, a second line associated with the same format F2 from one configuration tool to the next, a third line associated with the same format F3 from one configuration tool to the next, etc.
Such a display invariability within an interactive configuration tool from one screen to another facilitates and accelerates the search for the desired display format by the user when he seeks to change the current display configuration, and reduces the risk of entry error of his choice.
In relation with
In other words, on one or several screens E1, E2, E3, . . . , EN of the plurality of screens of the cockpit GC of
According to the example of
According to one particular aspect of the invention, the surface of the predetermined temporary display zone, like that of the predetermined permanent display zone ZP, is strictly smaller than half of the surface of the screen E1. According to the present invention, the same is true for any configuration tool, in other words, the surface of the predetermined display zone of a configuration tool is always strictly less than half of the surface of each screen of the plurality of screens of the glass cockpit.
Additionally, the location of the predetermined temporary display zone ZT like that of the predetermined permanent display zone ZP, on the screen E1, is separate from the location of a zone dedicated to the display of the information essential for the piloting of the vehicle, the location of the predetermined temporary display zone Z1, like that of the predetermined permanent display zone ZP, depending on the current display configuration of the screen E1.
In other words, the location and the size of the predetermined temporary display zone ZT (that is to say, appearance/disappearance for a temporary display) is optimized so as to limit the masking of the formats, in particular avionic in the process of retrieval.
According to one variant that is not shown, the configuration tool O1 is displayed by superposition, thus making it possible to see the retrieved video stream below.
In
The position (that is to say, location within the screen E1) of the temporary display zone ZT is adapted such that it does not hide the primary control parameters. Thus, in
Thus, even if the configuration tool O1 is displayed temporarily in the temporary display zone ZT (that is to say, several seconds), it is possible for the pilot of the aircraft to continue to monitor the parameters essential to his task, namely piloting, continuously.
Likewise, according to the configuration tool O1 of
Furthermore, compared to the configuration tool O1 of
Furthermore, the configuration tool O1 of
As an alternative to the entry symbol 12 comprising a second additional signal element, a dedicated entry symbol with an explicit mention such as “BACK” can be added within a configuration tool according to the present invention.
As illustrated by
Such a predetermined permanent display zone ZP for example comprises a banner, the width of which makes it possible to display a single user entry symbol per format, which is why reference is made to shortened or reduced permanent display relative to the complete temporary display, in particular with three user entry symbols per format, of the same configuration tool O1.
Such a shortened permanent display makes it possible to reduce the graphic footprint (that is to say, the size) of the permanent display of the display configuration tool in order to optimize the size of the remaining surface of the considered screen dedicated to the display of the avionic format(s) to be retrieved on this screen, while offering the user the possibility of continuously viewing, with immediate access, the format(s) in the process of being retrieved, namely, in
Such a banner is for example located adjacent to one or several of the sides of the screen and inside the considered screen.
According to the example of
According to another example, not shown, the permanent banner is able to retrieve only a predetermined subset of the display configurations available in the configuration tool O1 displayed temporarily superimposed on the screen, such a permanent banner subset being able to differ from one screen to another, like the order of the display configurations of such a permanent banner subassembly. From such a permanent banner, the temporary display of the configuration tool O1 in the temporary display zone ZT is for example activated by tactile pressure in the banner, that is to say, the predetermined permanent display zone ZP.
According to another example, not shown, a dual display of permanent banners (that is to say, on both the left and right sides of the considered screen) is implemented.
According to one particular aspect, when the interactive display configuration tool is configured to be temporarily displayed, the display device is configured to close automatically, the configuration tool O1 displayed in the temporary display zone Z1, after activation of a user entry symbol (the activation being equivalent to selection of a new display configuration to be applied), and/or after expiration of a predetermined time period, and/or after detection of a user entry outside the predetermined display zone ZT of the configuration tool (for example in case of user entry on a screen other than the screen E1 or by new mechanical pressure on the dedicated button of the screen that activated the display of the configuration tool).
One non-limiting example of operation of the display device according to the invention will now be explained using
During a first step 22 of such a display method 20, the display device is for example activated by receiving R a manual mechanical pressure on a dedicated button of one of the screens of the glass cockpit. According to other examples, such an activation of the display device is done via the tactile pressure or the pointing of a virtual button of the considered screen or the entry of a predetermined tactile gesture on the surface of said screen.
During a following step 24, the display device performs the display A of the configuration tool locally on this screen.
During a following step 26, the display device receives the entry S of the display configuration selected by the user by pressing of the desired user entry symbol.
During a following step 28, the display device implements the modification M of the current display configuration according to the display configuration previously selected by the user, and in case of selection of a user entry symbol different from the user entry symbol corresponding to the current display configuration. In other words, the retrieved format is different before and after step 28.
During a final step 30, the display device closes F the configuration tool. Such closing is done either automatically before expiration of a predetermined time period, or manually by pressure outside the configuration tool, or by pressure on the mechanical or virtual button used to open the configuration tool.
One can thus see that the display device according to the present invention allows the pilot to adapt, effectively, intuitively and while limiting the risk of errors, the display configuration of his cockpit as a function of the task/mission that he must perform.
Such effectiveness is in particular obtained via a configuration tool associated with each screen of the glass cockpit of the cockpit and locally displayable on the screen that is specific thereto, each configuration tool comprising a set of explicit user entry symbols so that the pilot uses them to select the desired display configuration.
Furthermore, the display device according to the present invention is able to provide display coherence of configuration tools on the set of screens, and to optimize the size and the position of each configuration tool in order to locally limit, on each screen, the masking of avionic formats during retrieval, which allows the pilot to keep his attention on the essential parameters of the formats displayed for the time needed for the display reconfiguration task.
Furthermore, according to one particular aspect, in order to facilitate the use by the pilot and the effectiveness of the reconfiguration task, the order of the display formats of the configuration tool displayed temporarily is the same over all of the screens of the cockpit. Nevertheless, normative or technical constraints can impose or prevent certain display configurations. In order for the pilot not to be required to know these constraints in order to understand the behavior of the system (which would result in complicating his task, therefore potentially increasing his workload, or even in some situations downgrading the safety of the operation if he must act urgently), the configuration tool explicitly shows the current display configuration on the screen associated with the configuration tool, the display configuration(s) that are displayable from the current display configuration, the display configuration(s) that are displayable at least once on the screen but are not displayable from the current display configuration, the display configuration(s) that are never displayable on the considered screen.
Number | Date | Country | Kind |
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19 08064 | Jul 2019 | FR | national |