Apparatus and method for aircraft display and control

• US 5,978,715 A
• Filed: 10/15/1997
• Issued: 11/02/1999
• Est. Priority Date: 10/15/1997
• Status: Expired due to Term

• Current Assignee: Dassault Aviation (Groupe Industriel Marcel Dassault)
• Original Assignee: Dassault Aviation (Groupe Industriel Marcel Dassault)
• Inventors: Mitaux-Maurouard, Guy, Briffe, Michel
• Primary Examiner(s): Cuchlinski, Jr., William A.
• Assistant Examiner(s): ARTHUR JEANGLAUDE, GERTRUDE
• Application Number:
  US08/950,762
• Time in Patent Office: 748 Days
• Field of Search: 701/1, 701/11, 701/13, 701/14, 701/15, 701/16, 244/158 R, 244/75 R, 244/176
• US Class Current: 701/11
• CPC Class Codes: G01C 23/00 Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration
• CPC Class Codes: G05D 1/0808 specially adapted for aircraft

Abstract

An aircraft flight deck includes a primary flight display device and a combined autopilot/autothrottle controller. The controller is mounted on the flight panel below the windshield in a vertical line with the primary flight display. A thumb-activated multiaxis control switch is mounted on the control yoke and operates exclusively to adjust a preselected trajectory commanded to the autopilot when moved leftfright or fore/aft. Depressing the switch in a vertical axis in a position generates an ENABLE signal to activate the commanded preselected trajectory.

Claims

1. Interface apparatus for an aircraft which includes a primary flight parameter display unit and a windshield, comprising:

an automatic control unit with a plurality of control modes for controlling at least one of vertical, horizontal, and speed flight parameters and for generating display signals indicative of selected and selectable modes and warning conditions;

an interface panel physically located between the windshield and the primary flight director display unit;

a display area associated with the interface panel and coupled to the automatic control unit for displaying the display signals;

a control device located in the interface panel for receiving pilot-entered selections of the control modes and coupled to the automatic control unit for transmitting the control mode selections to the automatic control unit.

2. Apparatus as recited in claim 1, wherein the control device is overlying the display area.

3. Apparatus as recited in claim 2, wherein the display area and the control device comprise a touch-sensitive screen.

4. Apparatus as recited in claim 1, wherein the automatic control unit comprises an autopilot.

5. Apparatus as recited in claim 4, wherein the automatic control unit comprises an autopilot having a plurality of sub-modes.

6. Apparatus as recited in claim 5, wherein the autopilot automatically generates signals to:

control flight parameters to cause the aircraft to follow a flight path specified by published named procedures, and

to cause the display area to display the name of the procedure currently being executed.

7. Apparatus as recited in claim 1, wherein the automatic control unit comprises an autothrottle.

8. Apparatus for controlling an aircraft having multiple control surfaces, comprising:

a control handle for supplying pilot-entered manual inputs to the control surfaces to initiate a change in aircraft attitude;

an automatic control unit for receiving at least one of roll, pitch and yaw signals to establish a desired aircraft trajectory and for supplying at least one of roll, pitch and yaw signals to the control surfaces to maintain the aircraft on the desired trajectory; and

a multi-position switch mounted on the control handle exclusively for generating commands in response to pilot input to selectively increase and decrease the at least one of roll, pitch and yaw signals supplied to the automatic control unit;

thereby changing the desired trajectory.

9. Apparatus as recited in claim 8, wherein the automatic control unit generates displays to communicate required manual control inputs to achieve a desired trajectory.

10. Apparatus for controlling an aircraft having multiple control surfaces, comprising:

a control handle for supplying pilot-entered manual inputs to the control surfaces to initiate a change in aircraft attitude;

an automatic control unit for receiving signals to establish a desired aircraft trajectory and for supplying signals to the control surfaces to maintain the aircraft on the desired trajectory; and

a multi-position switch mounted on the control handle for generating commands in response to pilot input to selectively increase and decrease the signals supplied to the automatic control unit;

thereby changing the desired trajectory, wherein the multi-position switch comprises a first momentary-contact activation axis having first and second switch contacts for respectively generating INCREASE and DECREASE commands, a second momentary-contact activation axis having first and second switch contacts for respectively generating INCREASE and DECREASE commands, and a third momentary-contact activation axis having a single switch contact;

the first, second, and third axes being mutually perpendicular.

11. Apparatus for controlling an aircraft having multiple control surfaces, comprising:

a control handle for supplying pilot-entered manual inputs to the control surfaces to initiate a change in aircraft attitude;

an automatic control unit for receiving signals to establish a desired aircraft trajectory and for supplying signals to the control surfaces to maintain the aircraft on the desired trajectory; and

a multi-position switch mounted on the control handle for generating commands in response to pilot input to selectively increase and decrease the signals supplied to the automatic control unit;

thereby changing the desired trajectory;

wherein the automatic control unit stores the commands generated by the switch without activating the entered change in desired trajectory; and

wherein the switch comprises a switch position for receiving a pilot-entered ENABLE signal to activate the entered change in desired trajectory.

12. Apparatus as recited in claim 11, comprising a display unit connected to the storing means for graphically displaying a representation of the change in trajectory commanded by inputs to the switch.

13. Apparatus as recited in claim 12, wherein the display unit displays a first representation of the change in trajectory commanded by inputs to the switch prior to entry of an ENABLE signal and a second representation of the change in trajectory commanded by inputs to the switch after entry of an ENABLE signal.

14. A method for controlling an aircraft having multiple control surfaces for changing aircraft attitude in response to pilot-entered manual inputs supplied to a control handle and to signals from an autopilot, comprising the steps of:

supplying signals from the autopilot to the control surfaces to maintain the aircraft on a desired trajectory;

generating commands in response to pilot input to a multi-position switch mounted on the control handle to selectively supply INCREASE and DECREASE signals to the autopilot;

thereby establishing a proposed new desired trajectory;

storing without activating the proposed new desired trajectory;

generating an ENABLE signal in response to a pilot-entered input to the multi-position switch; and

activating the proposed new trajectory as the desired trajectory in response to the ENABLE signal.