Display system and method for an aircraft
The display system for an aircraft cockpit comprises a display computer configured to control the display, on a display device worn rigidly attached to a user's head, according to a first display mode comprising at least one piece of flight assistance information for the aircraft, and a masking device, associated with a cockpit side window, controllable between a transparent and opaque states. The display system comprises an extended display mode, in which the display computer is configured to determine whether a direction corresponding to the user's head orientation has an intersection with a region of interest of the side window, in the absence of an intersection, controlling the display according to the first display mode, and when there is an intersection, controlling the masking device opaque state and controlling the display according to a second display mode comprising a virtual display screen on a side window display area.
1. A display system for a cockpit of an aircraft, the said display system comprising:
a display device configured to be worn rigidly attached to a user's head in the cockpit of the aircraft; and
a display computer configured for controlling the display on the display device according to a first display mode in which the display comprises at least one piece of flight assistance information for the aircraft relating to a current situation of the aircraft,
a masking device associated with a side window of the cockpit, the masking device being controllable between a first state called transparent in which the masking device allows the user to see an environment outside of the aircraft through the side window and a second state called opaque in which the masking device masks a view of the environment outside of the aircraft from the user through at least one predetermined masking surface of the side window;
a device for enabling an extended display mode, wherein the display computer is further configured to enable or disable the extended display mode according to actions of the user on the device for enabling the extended display mode; and,
a sensor for position and for orientation of the head of the user in the cockpit, and
wherein in extended display mode the display computer is configured for:
acquiring from the sensor, position information and orientation information on the head of the user in the cockpit;
determining a direction corresponding to the orientation of the head of the user as a function of the information on position and on orientation of the head of the user in the cockpit;
determining whether the direction corresponding to the orientation of the head of the user has an intersection with a region of interest including an area referred to as display area included within the predetermined masking surface of the side window;
when the direction corresponding to the orientation of the head of the user does not have an intersection with the region of interest, controlling the display on the display device according to the first display mode; and
only when the direction corresponding to the orientation of the head of the user has an intersection with the region of interest, and when the extended display mode has been enabled, controlling the masking device to be in the second state and controlling the display on the display device according to a second display mode in which the said display comprises a virtual display screen on the display area.
2. The system according to claim 1 , the display computer being configured for:
acquiring, from an avionics computer of the aircraft, information on a current flight phase of the aircraft; and
when the information on the current flight phase of the aircraft corresponds to a predetermined flight phase, controlling the opaque state of the masking device only when the extended display mode is enabled and when the direction corresponding to the orientation of the head of the user has an intersection with the region of interest.
3. The system according to claim 1 , wherein, in the second display mode, the display computer is furthermore configured for:
determining a distance between a current position of eyes of the user and the display area of the side window; and
controlling the display of the said virtual display screen on the display device with a collimation distance substantially corresponding to the distance determined between the current position of the eyes of the user and the side window display area.
4. The system according to claim 1 , further comprising a connection at an input to a device of an EFB type and, in the second display mode, the display on the virtual display screen corresponding to information coming from the device of the EFB type.
5. A display method for a cockpit of an aircraft, the aircraft comprising a display system comprising:
a display device configured so as to be worn rigidly attached to a user's head in the cockpit of the aircraft; and
a display computer configured for controlling the display on the display device according to a first display mode in which the display comprises at least one piece of flight assistance information for the aircraft relating to a current situation of the aircraft,
a masking device associated with a side window of the cockpit, the masking device being controllable between a first state called transparent in which the masking device allows the user to see an environment outside of the aircraft through the side window and a second state called opaque in which the masking device masks a view of the environment outside of the aircraft from the user through at least one predetermined masking surface of the side window;
a device for enabling an extended display mode, wherein the display computer is further configured to enable or disable the extended display mode according to actions of the user on the device for enabling the extended display mode; and
a sensor for position and for orientation of the head of the user in the cockpit,
wherein in extended display mode of the display system, the method comprises the following steps implemented by the display computer:
acquiring, from the sensor, position information and orientation information on the head of the user in the cockpit;
determining a direction corresponding to the orientation of the head of the user as a function of the information on position and on orientation of the head of the user in the cockpit;
determining whether the direction corresponding to the orientation of the head of the user has an intersection with a region of interest including an area referred to as display area included in the predetermined masking surface of the side window;
when the direction corresponding to the orientation of the head of the user does not have an intersection with the region of interest, controlling the display on the display device according to the first display mode; and
only when the direction corresponding to the orientation of the head of the user has an intersection with the region of interest, and when the extended display mode has been enabled, controlling the masking device to be in the second state and controlling the display on the display device according to a second display mode in which the said display comprises a virtual display screen on the display area.
6. An aircraft comprising a display system according to claim 1 .
7. The display method of claim 5 , wherein the process further comprises:
acquiring, from an avionics computer of the aircraft, information on a current flight phase of the aircraft; and
when the information on the current flight phase of the aircraft corresponds to a predetermined flight phase, controlling the opaque state of the masking device only when the extended display mode is enabled and when the direction corresponding to the orientation of the head of the user has an intersection with the region of interest.