Aircraft flight control
The invention described herein provides a flight crew with an easier and more intuitive way to control and monitor flight-control surfaces. Specifically, the invention displays all flight-control surfaces on a touch-screen display device located in an aircraft cockpit. The invention includes graphical and numerical position indicators to continuously display actual position information for flight-control surfaces. Additionally, the invention allows a flight crew to make flight-control surface adjustments through the touch-screen device. The invention further includes an engine performance indicator and a mode controller configured to display autopilot modes and to receive autopilot mode selections. A method is presented for controlling an aircraft flight-control surface via a touch screen device. The method includes receiving an indication of a flight-control surface and enabling selection of a position change. Based on the position change selection, the method includes verifying a corresponding movement and displaying an actual position of the flight-control surface.
1. A flight-control system for navigation of an aircraft, comprising:
a storage component having one or more instructions stored thereon;
a touch screen display device;
a processor coupled to the display device and a memory, the processor configured to execute the one or more instructions stored in the storage component; and
a manager configured to provide flight-control surface representations via the touch screen display device in an aircraft cockpit, the manager comprising:
a graphical image of the aircraft for displaying flight-control surface representations; and
one or more position indicators for indicating one or more positions of the aircraft flight-control surfaces,
wherein the graphical image and the position indicators are configured to receive indications for controlling positions of the aircraft flight-control surfaces and to continuously display actual aircraft flight-control surface positions via sensor measurements.
2. The system of claim 1 , wherein the aircraft flight-control surface includes an elevator and its position indicator indicates a nose-down or nose-up pitch of the elevator.
3. The system of claim 1 , wherein the aircraft flight-control surface includes a rudder and its position indicator indicates a left or right angle of the rudder.
4. The system of claim 1 , further comprising:
a graphical representation of aircraft wings for displaying wing flight-control surfaces; and
a second set of position indicators for indicating positions of the wing flight-control surfaces,
wherein the wing graphical representation and the second set of position indicators are configured to receive indications for controlling positions of the wing flight-control surfaces and to continuously display actual wing flight-control surface positions via sensor measurements.
5. The system of claim 4 , wherein the wing flight-control surface includes one or more ailerons and their respective position indicators indicate an up or down angle of the one or more ailerons.
6. The system of claim 4 , wherein the wing flight-control surface includes flaps and their respective position indicators indicate flap angles.
7. The system of claim 1 , wherein the position indicators include numerical and graphical indicators.
8. The system of claim 1 , further comprising one or more warning signals displayed by the graphical representation and position indicators.
9. The system of claim 8 , wherein the graphical representation and position indicators are configured to receive selections of options for responding to the one or more warning signals.
10. A flight-control system for navigation of an aircraft, comprising:
a storage component having one or more instructions stored thereon;
a touch screen display device;
a processor coupled to the display device and a memory, the processor configured to execute the one or more instructions stored in the storage component; and
a manager configured to provide autopilot controls and engine indicators via the touch screen display device in an aircraft cockpit, the manager comprising:
a cross-sectional representation of the aircraft fuselage for displaying a mode controller, wherein the mode controller is configured to display autopilot modes and to receive autopilot mode selections; and
the cross-sectional representation further including one or more engine cowls attached to the fuselage for continuously displaying performance indicators for the one or more engines.
11. The system of claim 10 , wherein the mode controller includes display options for receiving selections of autopilot, altitude, flight director, vertical navigation, vertical speed, and flight level change.
12. The system of claim 10 , wherein the cross-sectional representation of the aircraft fuselage with one or more engine cowls is located near a middle of the touch-screen instrument panel for receiving selections from either a pilot or a co-pilot.
13. The system of claim 10 , wherein the performance indicators include interstage turbine temperature for each of the one or more engines.
14. The system of claim 10 , wherein the performance indicators include fan speed for each of the one or more engines.
15. The system of claim 10 , wherein the indicators of engine performance display warnings of anomalous performance.
16. The system of claim 15 , wherein the indicators of engine performance are configured to receive selections of options for alleviating the anomalous performance.
17. A method for controlling an aircraft flight-control surface via a touch screen device comprising:
presenting a list of menu options on a touch screen mounted in an aircraft cockpit, said list including a flight-control function;
receiving a selection of the flight-control function;
upon selection of the flight-control function, receiving an indication of a flight-control surface to control;
upon identifying the flight-control surface, enabling selection of a position change; and
based on the position change selection, verifying a corresponding movement of the flight-control surface to the selected position.
18. The method of claim 17 , wherein the flight-control surface identified is one of a horizontal stabilizer, an elevator, a rudder, an aileron, a speed brake, a slat, or a flap.
19. The method of claim 17 , further comprising displaying a warning signal to indicate if the selected position of the control surface deviates from the actual position of the control surface.
20. The method of claim 19 , wherein the displayed warning signal presents a list of possible responses to the warning signal and receives an indication of a selected response to the warning signal.