This application is a National Stage of International patent application PCT/EP2017/057216, filed on Mar. 27, 2017, which claims priority to foreign French patent application No. FR 16/00545, filed on Apr. 1, 2016, the disclosures of which are incorporated by reference in their entirety.
The field of the invention is that of secure touch interfaces that are used notably in the avionics field as human-system interfaces.
One of the specific features of the aeronautical sector is that each display parameter and each interaction that a pilot is able to perform with the avionic system is defined by a ‘safety’ level of criticality that defines the criteria regarding integrity and availability of the hardware. For example, the level called ‘hazardous’ integrity level requires a probability of error of less than 10−7 per flight hour. Critical interactions have been performed, up until now, using dedicated control panels having the correct integrity level. For reasons regarding manufacturing and maintenance costs, but also for reasons regarding bulk, weight and electrical consumption, aviators are looking to reduce the number of control housings and to replace them with virtual equivalents that are displayed on the large touch-surface viewing screens of cockpits.
However, the essential condition for a control housing to be able to be ‘virtualized’ within a main screen is that this screen has at least the same level of criticality as the control housing that it is replacing. The inherent reliability of the components of a viewing screen means that the latter does not allow direct generation of highly critical commands. Thus, it is not possible simply to replace the action on one or more critical control buttons with a similar action on a touch surface.
Touch interaction means, notably capacitive ones, offer the option of performing a complex gesture able to be identified by the touchscreen, where a simple button allows only pressing and release functions to be applied. Thus, document U.S. Pat. No. 8,046,721, entitled ‘Unlocking a device by performing gestures on an unlock image’, proposes unlocking an electronic device by performing a particular ‘gesture’.
However, an arbitrary gesture does not make it possible to ensure the required reliability. Specifically, some simple faults with the touch surface may have the same effect as a simple gesture. This is the case with what are called ‘untimely’ presses. The touchscreen sends an item of information without any press from the user. This item of information may correspond to an isolated press or a succession of presses on a row or a column. This is also the case with what are called ‘erroneous’ presses. When pressing on the screen, the latter sends incorrect coordinates that do not match the actual location of the press. Thus, the fault with the touchscreen may simulate simple gestures, such as a simple press, a long press, a press along a row or a column, and thus generate incorrect commands, which is not acceptable.
To solve this problem, in existing interactive systems, when it is desired to ensure that the interaction has indeed been requested by a user and does not result from a fault, what is called the ‘guard’ principle is used. This principle is implemented on mechanical control buttons that require a high degree of security. It consists in protecting the control button by way of a cover. The button is able to be used only after the cover has been lifted. This principle may be transposed to touch commands. As illustrated in
The method for the secure control of a function by way of a touchscreen according to the invention does not exhibit these drawbacks. More precisely, the subject of the invention is a method for the secure control of an apparatus by way of a system comprising a viewing device comprising a touch surface formed of a matrix of conductive rows and columns, a viewing screen and a processing and control unit for said apparatus, said processing unit comprising a first assembly for processing positioning information coming from the touch surface and a second assembly for displaying graphical symbols on the viewing device, said secure control method comprising at least the following steps:
Advantageously, the pattern is in the shape of a V or an inverted V.
Advantageously, a path, contained within the pattern, is shown by a third symbol linking the first symbol to the second symbol.
Advantageously, the second symbol is displayed only when the first symbol is called upon by being touched.
Advantageously, the first symbol and the second symbol are shown differently depending on whether the apparatus is in the first state or the second state.
The invention will be better understood and other advantages will become apparent on reading the following description, which is given by way of nonlimiting example, and by virtue of the appended figures in which:
By way of nonlimiting example,
The viewing screen is generally a flat liquid-crystal display screen. This touch medium-viewing screen assembly is connected to a calculating unit 13, which performs the following functions:
Generating the various graphical depictions of the symbols for the viewing device;
Comparing the information coming from the touch controller with a pre-recorded control mechanism;
Generating information for controlling the system 20.
As has been stated, the reliability of touch systems, although it is excellent, may prove to be insufficient for certain highly secure applications, in particular in the case of untimely or erroneous presses. By way of example, in the aeronautical field, when the reliability of the control corresponds to a level of loss of integrity of less than 10−7 per flight hour, a simple control method is no longer sufficient.
To mitigate these drawbacks, the secure control method according to the invention comprises a plurality of steps that are illustrated in
Displaying a first symbol 30 corresponding to shutting down the apparatus and a second symbol 31 corresponding to putting the apparatus into service, the apparatus initially being shut down. It should be noted that the second symbol may be displayed only when the first symbol is called upon. By way of example, in
Putting the apparatus into service by way of a single continuous press on the touch surface starting on the first symbol 30, passing through a first crossing point 32 situated at the first symbol, following a pattern 34, passing through a second crossing point 33 situated at the second symbol 31 and finishing on the second symbol. It should be noted that the crossing points and the pattern are not displayed. This putting into service is shown in
Shutdown of the apparatus by the reverse method. The user performs a continuous press on the touch surface starting on the second symbol 31, passing through the second crossing point 33, following the path 35, passing through the first crossing point 32 and finishing on the first symbol 30.
By this simple means, during the putting into service, the touch surface sends to the touch controller only information corresponding to successive touch coordinates, corresponding to both different rows and columns and press/release information. The shape of the template is not able to be reproduced by a simple fault with a component of the touch surface. The absence of detection of simple faults by the system is thus avoided, and the reliability of the touch medium is increased significantly.
This method is particularly well-suited to the putting into service of apparatuses requiring a high degree of security. In the avionic field, this method allows the performance of interactions with what is called a ‘hazardous’ level of criticality.
Number | Date | Country | Kind |
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16 00545 | Apr 2016 | FR | national |
Filing Document | Filing Date | Country | Kind |
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PCT/EP2017/057216 | 3/27/2017 | WO | 00 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2017/167698 | 10/5/2017 | WO | A |
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Number | Date | Country |
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2 731 002 | May 2014 | EP |
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Number | Date | Country | |
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20190114068 A1 | Apr 2019 | US |