Autopilot/flight director underspeed protection system

• US 5,746,392 A
• Filed: 05/15/1995
• Issued: 05/05/1998
• Est. Priority Date: 05/15/1995
• Status: Expired due to Term

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Gast, Mark E.
• Primary Examiner(s): Mojica, Virna Lissi
• Application Number:
  US08/441,468
• Time in Patent Office: 1,086 Days
• Field of Search: 244/76 B, 244/178, 244/181, 244/182, 244/186, 244/194, 244/193, 244/195, 364/426.041, 364/431.07, 364/432
• US Class Current: 244/76.00B
• CPC Class Codes: B64C 13/16 actuated automatically, e.g. responsive to gust detectors
• CPC Class Codes: B64C 13/503 Fly-by-Wire
• CPC Class Codes: G05D 1/0607 specially adapted for aircraft

Abstract

An underspeed protection system for an aircraft under autopilot control selects a target speed based upon the greater of a minimum maneuver speed and a stick shaker speed. The system then compares a monitored speed to the target speed to produce an error signal. The system also monitors vertical speed to determine if the aircraft begins to descend. If the error signal due to the underspeed condition causes the aircraft to descend, the system provides a hold zero vertical speed signal in place of the error signal such that the aircraft seeks to maintain its altitude. The hold zero vertical speed signal overrides the underspeed error signal such that the aircraft does not pitch forward to seek an increased speed.

Claims

1. A method of limiting underspeed in an aircraft having flaps, comprising the steps of:

selecting a set of flight parameters;

determining a target speed of the aircraft;

determining an actual speed of the aircraft;

comparing the target speed to the actual speed;

producing an electrical first error signal indicative of the difference between the actual speed and the target speed;

monitoring a flap position of the flaps;

adjusting the first error signal in response to the monitored flap position;

receiving the adjusted first error signal with an electronic controller; and

adjusting the selected set of flight parameters with the electronic controller in response to the adjusted first error signal.

14. The method of claim 1 wherein the step of determining an actual speed of the aircraft includes monitoring the airspeed with a first airspeed monitor, further comprising the steps of:

determining a second airspeed with a second airspeed monitor separate from the first airspeed monitor;

comparing the second airspeed to the target speed;

producing a second error signal indicative of the difference between the second airspeed and the target airspeed;

receiving the second airspeed with the electronic controller; and

adjusting the selected set of flight parameters in response to the second error signal.

17. The method of claim 1 wherein the step of determining a target speed comprises the steps of:

selecting a minimum maneuver speed for the aircraft;

selecting a safety margin; and

adding the safety margin to the minimum maneuver speed to produce the target speed.

2. A method for limiting underspeed in an aircraft under autopilot control, the autopilot establishing a set of flight control parameters to seek a selected flight condition of the aircraft, comprising the steps of:

selecting a nominal minimum maneuver speed for the aircraft;

selecting a target speed relative to the minimum maneuver speed;

determining an actual speed of the aircraft;

comparing the actual speed to the target speed;

if the determined actual speed of the aircraft is below the target speed, producing a first underspeed signal;

supplying the first underspeed signal to an electronic flight controller;

in response to the first underspeed signal, overriding the set of flight control parameters with the flight controller by supplying a revised set of flight control parameters to seek a revised flight condition in which the actual speed of the aircraft approaches the target speed; and

after overriding the set of flight control parameters, maintaining the revised set of flight control parameters until either the autopilot is disengaged or a new set of flight control parameters is selected by a pilot.

15. The method of claim 2 further comprising the steps of:

monitoring a flap position of the aircraft; and

amplifying the first underspeed signal with a gain unresponding to the monitored flap position.

16. The method of claim 2 wherein the step of determining the actual speed includes the step of

calculating an airspeed of the aircraft, further comprising the steps of

monitoring the airspeed;

comparing the monitored airspeed to the target speed;

if the monitored airspeed is below the target speed, producing a second underspeed signal; and

supplying the second underspeed signal to the electronic flight controller

wherein the step of overriding the set of flight control parameters with the flight controller by supplying a revised set of flight control parameters to seek a revised flight condition in which the calculated airspeed of the aircraft approaches the target speed is responsive to the second underspeed signal.

3. A method for limiting underspeed in an aircraft under autopilot control, the autopilot establishing a set of flight control parameters to seek a selected flight condition of the aircraft, comprising the steps of:

selecting a nominal minimum maneuver speed for the aircraft;

selecting a target speed relative to the minimum maneuver speed;

determining an actual speed of the aircraft;

comparing the actual speed to the target speed;

if the determined actual speed of the aircraft is below the target speed, producing a first underspeed signal;

supplying the first underspeed signal to an electronic flight controller; and

in response to the first underspeed signal, overriding the set of flight control parameters with the flight controller by supplying a revised set of flight control parameters to seek a revised flight condition in which the actual speed of the aircraft approaches the target speed; and

wherein the step of selecting a minimum maneuver speed includes the steps of;

selecting a stick shaker speed for a monitored flight condition;

selecting a safety margin; and

adding the safety margin to the stick shaker speed to determine a stick shaker-based minimum speed.

4. The method of claim 3 wherein the step of selecting a nominal minium speed further includes the steps of:

determining a monitored airspeed-based minimum speed for the monitored flight condition;

comparing the monitored airspeed-based minimum speed to the minium maneuver speed;

selecting the greater of the monitored airspeed-based minimum speed and the stick shaker-based minimum speed; and

setting the minimum maneuver speed equal to the selected greater speed.

5. A method for limiting underspeed in an aircraft under autopilot control, the autopilot establishing a set of flight control parameters to seek a selected flight condition of the aircraft, comprising the steps of:

selecting a nominal minimum maneuver speed for the aircraft;

selecting a target speed relative to the minimum maneuver speed;

determining an actual speed of the aircraft;

comparing the actual speed to the target speed;

if the determined actual speed of the aircraft is below the target speed, producing a first underspeed signal;

supplying the first underspeed signal to an electronic flight controller; and

in response to the first underspeed signal, overriding the set of flight control parameters with the flight controller by supplying a revised set of flight control parameters to seek a revised flight condition in which the actual speed of the aircraft approaches the target speed, wherein the step of selecting a target speed relative to the minimum maneuver speed includes the step of adding a speed margin to the minimum maneuver speed, and wherein the step of producing a first underspeed signal includes the step of producing a signal proportional to the difference between the actual speed and the target speed.

6. The method of claim 5, further including the steps of:

if the actual speed of the aircraft falls below the target speed, producing a second underspeed signal proportional to the difference between the actual speed and the target speed; and

filtering the second underspeed signal to produce a filtered underspeed signal wherein the step of overriding the set of flight control parameters is responsive to both the first and filtered underspeed signals.

7. A method for controlling descent in an aircraft under autopilot control, the autopilot establishing a set of flight control parameters to seek a selected flight condition of the aircraft, comprising the steps of:

selecting a nominal minimum maneuver speed for the aircraft;

selecting a target speed relative to the minimum maneuver speed;

monitoring an actual speed of the aircraft;

establishing a hold zero vertical speed set of flight parameters;

comparing the actual speed to the target speed;

if the actual speed of the aircraft is below the target speed, producing a first underspeed signal;

supplying the first underspeed signal to an electronic flight controller;

in response to the first underspeed signal, determining a revised set of flight control parameters;

determining a response of the aircraft to the revised set of flight control parameters;

if the revised set of flight control parameters causes the aircraft to descend, overriding the set of flight control parameters with the flight controller by supplying to the hold zero vertical speed set of flight control parameters to the autopilot; and

if the revised set of flight control parameters does not cause the aircraft to descend, overriding the set of flight control parameters with the flight controller by supplying to the revised set of flight control parameters to the autopilot.

8. The method of claim 7, further including the step of:

after supplying the revised set of flight control parameters or the hold zero vertical speed set of flight control parameters to the autopilot, maintaining the revised set of flight control parameters or the hold zero vertical speed set of flight control parameters until either the autopilot is disengaged or a new set of flight control parameters is selected by a pilot.

9. The method of claim 8 wherein the step of selecting a minimum maneuver speed includes the steps of:

selecting a stick shaker speed for a monitored flight condition;

selecting a safety margin; and

adding the safety margin to the stick shaker speed to determine a stick shaker-based minimum speed.

10. The method of claim 8 wherein the step of producing a first underspeed signal includes the step of producing a signal proportional to the difference between the actual speed and the target speed.

11. The method of claim 10, further including the steps of:

if the actual speed of the aircraft falls below the target speed, producing a second underspeed signal proportional to the difference between the actual speed and the target speed; and

filtering the second underspeed signal to produce a filtered underspeed signal.

12. The method of claim 7 further comprising the steps of:

monitoring a flap position of the aircraft; and

amplifying the first underspeed signal in response to the monitored flap position.

13. The method of claim 7 further comprising the steps of:

calculating an airspeed of the aircraft;

comprising the calculated airspeed to the target speed;

if the calculated airspeed is below the target speed, producing a second underspeed signal;

supplying the second underspeed signal to the electronic flight controller; and

in response to the second underspeed signal, overriding the set of flight control parameters with the flight controller by supplying a revised set of flight control parameters to seek a revised flight condition in which the calculated airspeed of the aircraft approaches the target speed.