Flight control system and method for an aircraft circle-to-land maneuver

• US 6,438,469 B1
• Filed: 02/07/2000
• Issued: 08/20/2002
• Est. Priority Date: 02/07/2000
• Status: Expired due to Fees

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Maahs, Dave Charles, Dwyer, David Brandt
• Primary Examiner(s): Cuchlinski, Jr., William A.
• Assistant Examiner(s): Marc-Coleman, Marthe Y.
• Application Number:
  US09/498,676
• Time in Patent Office: 925 Days
• Field of Search: 701/16, 701/17, 701/18, 340/947, 340/948, 340/951, 340/945, 340/952, 340/972, 340/980, 340/981, 342/33, 342/34, 244/3.1, 244/3.23, 244/75.R, 244/183, 244/114.R
• US Class Current: 701/16
• CPC Class Codes: G05D 1/0676 specially adapted for landing
• CPC Class Codes: G08G 5/025 Navigation or guidance aids radar or analogous systems specially adapted for landing purposes G01S13/913

Abstract

A flight control system and method for controlling a circle-to-land (“CTL”) maneuver utilizes an airborne area navigator. The area navigator receives inputs on aircraft category, aircraft position and speed, airport navigation data and pilot supplied data. In response to this data, the area navigator calculates the necessary conditions for executing the CTL maneuver and outputs control commands to a flight director. The pilot then executes the CTL maneuver either manually using the information provided by the area navigator or by using the aircraft autopilot under the direction of the flight director.

Claims

1. A method for landing an aircraft on a designated runway at a predetermined airport including executing a circle-to-land maneuver comprising the steps of:

selecting a standard terminal arrival path;

directing the aircraft to a starting point of a standard terminal arrival path;

following the standard terminal arrival path to a first waypoint for initiation of the circle-to-land maneuver; and

allowing an airborne area navigator system to calculate and to control the circle-to-land maneuver including a downwind leg to a second waypoint and a base leg to a third waypoint to align the aircraft with a final leg directed to the designated runway.

2. The method of claim 1 wherein the step of following the standard terminal arrival path to a first waypoint comprises directing the aircraft to a location along a line positioned substantially at the end of and perpendicular to the end of the runway.

3. The method of claim 1 wherein the step of allowing comprises determining an appropriate ground track including a 180 degree turn from the downwind leg to the final leg.

4. The method of claim 1 wherein the step of allowing comprises calculating and controlling both the lateral and vertical path of the aircraft.

5. The method of claim 1 further comprising the step of entering pilot-selected data into the airborne area navigator.

6. The method of claim 5 wherein the step of entering comprises entering information concerning aircraft category and minimum descent altitude.

7. The method of claim 6 wherein the step of allowing comprises calculating and controlling to maintain the aircraft within protected airspace.

8. The method of claim 5 wherein the step of entering comprises entering data selected from preference for a right turn or a left turn direction, turn radius, final approach segment length, and final approach glidepath.

9. The method of claim 8 wherein the step of allowing comprises calculating and controlling a circle-to-land maneuver along a predetermined ground track determined in part by data entered.

10. A flight control system for automatically controlling a circle-to-land maneuver of an aircraft comprising:

an onboard area navigator;

sensors coupled to first inputs of the area navigator for inputting aircraft position and velocity data;

second inputs to the area navigator for receiving pilot-supplied data;

third inputs to the area navigator for receiving airport-specific data;

a flight director coupled to a first output of the area navigator to receive commands from the area navigator, the commands responsive to data received at the first, second, and third inputs;

an autopilot capable of controlling the flight of the aircraft;

a pilot-operable switch coupled between the flight director and the autopilot for selectively engaging the autopilot; and

an operator cockpit display coupled to a second output of the area navigator for providing flight information to a pilot, the information responsive to data received at the first, second, and third inputs.

11. The flight control system of claim 10 wherein the commands are selected from a list consisting of:

a pitch command, a speed command, and a roll steering command.

12. The flight control system of claim 10 wherein the flight information comprises deviations in aircraft vertical position, lateral position, and speed.

13. The flight control system of claim 10 wherein the pilot-supplied data comprises aircraft category.

14. The flight control system of claim 10 wherein the pilot-supplied data comprises desired turn radius, final approach length, and approach velocity for the circle-to-land maneuver.

15. The flight control system of claim 10 wherein the airport specific data comprises latitude, longitude, and elevation of the runway upon which the aircraft is to be landed.

16. An onboard flight control system for automatically controlling a circle-to-land maneuver of an aircraft comprising:

an onboard area navigator programmed to determine an appropriate circle-to-land maneuver in response to data supplied to the onboard area navigator;

inputs coupled to the onboard area navigator to convey the data to the onboard area navigator; and

a visual display coupled to an output of the onboard area navigator to display operating information to a flight crew aboard the aircraft, the operating information responsive to data received by the inputs.

17. The onboard flight control system of claim 16 wherein the onboard area navigator is programmed to include a vertical navigation subsystem.

18. The onboard flight control system of claim 17 wherein the vertical navigation subsystem of the onboard area navigator is adapted to receive data from an altitude preselector.

19. The onboard flight control system of claim 18 wherein the vertical navigation subsystem of the onboard area navigator is programmed to ignore the data from the altitude preselector during a circle-to-land maneuver.

20. The onboard flight control system of claim 16 further comprising a flight director coupled to an output of the onboard area navigator to convey operating information to a flight crew aboard the aircraft, the operating information responsive to data received by the inputs.

21. A method for executing a circle-to-land maneuver for an aircraft by utilizing area navigator and autopilot systems onboard an aircraft, the method comprising the steps of:

determining a runway selected for landing;

selecting an approach path for initiating the circle-to-land maneuver;

entering data concerning desired flight conditions into the area navigator to allow the area navigator to calculate lateral and vertical navigation required for the circle-to-land maneuver;

directing the aircraft to the waypoint at which the circle-to-land maneuver is to begin; and

allowing the autopilot, directed by the area navigator, to execute the maneuver from the waypoint to the selected runway.

22. The method of claim 21 wherein the step of entering data comprises entering minimum descent altitude, desired turn direction, turn radius, final approach segment length, and final approach glidepath angle.

23. The method of claim 22 wherein the step of entering data further comprises entering the aircraft category to allow the area navigator to calculate the appropriate circling maneuver to keep the aircraft within protected airspace.

24. A method for landing an aircraft on a designated runway at a predetermined airport including executing a circle-to-land maneuver, the method comprising the steps of:

providing an airborne area navigator system programmed to designate the ground track for the circle-to-land maneuver onto the designated runway at the predetermined airport;

designating a ground track for the circle-to-land maneuver;

providing instructions to the aircraft from the airborne area navigator system directing the aircraft to intercept the circle-to-land maneuver at an intercept predetermined by a flight crew aboard the aircraft;

upon intercept of the circle-to-land maneuver, allowing the airborne area navigator system to direct the aircraft to follow the ground track for the circle-to-land maneuver.

25. The method of claim 24 further comprising the step of providing from the airborne area navigator, instructions to the flight crew to navigate to the predetermined intercept.

26. The method of claim 24 wherein the step of providing instructions to the aircraft from the airborne area navigator system directing the aircraft to intercept the circle-to-land maneuver comprises providing instructions directing the aircraft to fly a base leg and a final leg.