System and method of using a multi-view display

An instrumentation system of an aircraft, comprising:

• a plurality of main sensors configured to measure a plurality of aircraft data;
• a plurality of standby sensors, separate from said plurality of main sensors, configured to measure the plurality of aircraft data;
• a processor to receive the plurality of aircraft data from said plurality of main sensors and said plurality of standby sensors;
• and
• a multi-view display in communication with said processor, said multi-view display and said processor configured to display a first image including at least one of the plurality of aircraft data and a second image including at least one of the plurality of aircraft data from said plurality of standby sensors at all times during operation of the aircraft;
• wherein the first image is displayed within a first viewing envelope associated
• with a first crew member of the aircraft and the second image within a second viewing envelope, different from the first viewing envelope, associated with a second crew member of the aircraft.

An instrumentation system of an aircraft, comprising:

• a plurality of first main sensors configured to measure a plurality of aircraft data;
• a plurality of second main sensors configured to measure a second plurality of aircraft data;
• a plurality of standby sensors separate from said plurality of first main sensors and the plurality of second main sensors configured to measure a third plurality of aircraft data;
• a first processor to receive the plurality of aircraft data from said plurality of first main sensors and said plurality of standby sensors;
• a second processor to receive the plurality of aircraft data from said plurality of second main sensors and said plurality of standby sensors;
• a first multi-view display in communication with said first processor, said first multi-view display and said first processor configured to display a first image including at least one of the plurality of aircraft data and a second image including at least one of the plurality of aircraft data from said plurality of standby sensors at all times during operation of the aircraft;
• wherein the first image is displayed within a first viewing envelope associated with a first crew member of the aircraft and the second image within a second viewing envelope, different from the first viewing envelope, associated with a second crew member of the aircraft;
• and
• a second multi-view display in communication with said second processor, said second multi-view display and said second processor configured to display a third image including at least one of the plurality of aircraft data and a fourth image including at least one of the plurality of aircraft data from said plurality of standby sensors at all times during operation of the aircraft;
• wherein the third image is displayed within a third viewing envelope associated with the second crew member of the aircraft and the fourth image within a fourth viewing envelope, different from the third viewing envelope, associated with the first crew member of the aircraft.