System for tanker entering rendezvous orbit

• US 20020193915A1
• Filed: 02/20/2002
• Published: 12/19/2002
• Est. Priority Date: 06/11/2001
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Miller, Ronald J.
• Granted Patent: US 6,678,587 B2
• Time in Patent Office: Days
• US Class Current: 701/3
• CPC Class Codes: G05D 1/0202 specially adapted to aircraft
• CPC Class Codes: G08G 5/0052 for cruising combined instruments indicating more than one navigational value G01C23/00

Abstract

A navigation and guidance computer system using navigation sensors to determine aircraft position, and automatically control the aircraft to fly from an initial position to intercept and follow a crew-selected rendezvous orbit in accordance with Air Traffic Control and military specified rules. It creates maneuvers that result in smooth, efficient motion of the aircraft from an initial position to the execution of a rendezvous orbit. It controls the aircraft by applying commands to the aircraft'"'"'s autopilot. The system creates the smooth and coordinated maneuvers by considering and anticipating all constraints on the aircraft flight path by creating a single maneuver that is a re-entry maneuver, an over fly maneuver, and a turning maneuver all as a single turn that is contained entirely within the allowable airspace. All maneuvers are created and executed recognizing the turning capability of the aircraft considering allowable bank angles, current wind conditions and true airspeed.

Claims

1. A method for maneuvering an aircraft for entering into a holding pattern, the aircraft position being known and the location and orientation of the holding pattern being known, the method comprising the steps of:

dividing an airspace around the holding pattern into at least three zones;

determining a relative bearing between a line from the aircraft to a control point of the holding pattern and an inbound leg line through the control point of the holding pattern;

selecting an entry zone from the at least three zones based on the determined relative bearing;

providing a predetermined entry maneuver for the selected entry zone; and

executing the predetermined entry maneuver.

2. The method of claim 1 wherein the at least three zones comprise:

a first zone comprising the relative bearing of an angle between −

180 degrees to <

0 degrees;

a second zone comprising the relative bearing of an angle between >

+90 degrees to <

+180 degrees; and

a third zone comprising the relative bearing of an angle between 0 to +90 degrees.

3. The method of claim 2 wherein second zone further comprises:

zone 2b comprising a portion of second zone that lies between the inbound leg and an outbound leg extended; and

zone 2a comprising a remaining portion of the second zone not within zone 2b.

4. The method of claim 3 wherein the step of providing a predetermined entry maneuver for zone 2a comprises:

initially flying toward the control point; and

turning to capture the outbound leg of the holding pattern.

5. The method of claim 4 wherein the step of turning to capture the outbound leg of the holding pattern comprises initiating the turn after intersecting the outbound leg.

6. The method of claim 3 wherein the step of providing a predetermined entry maneuver for zone 2b comprises:

initially flying toward the control point; and

initiating a turn to capture the outbound leg of the holding pattern at a distance from the control point equal to twice an aircraft'"'"'s worst case turning radius.

7. The method of claim 2 wherein the step of providing a predetermined entry maneuver for zone 1 comprises:

flying over the control point; and

capturing the outbound leg of the holding pattern.

8. The method of claim 7 wherein the step of flying over the control point comprises flying directly to and over the control point.

9. The method of claim 2 wherein the step of providing a predetermined entry maneuver for zone 3 comprises flying to intersect tangentially semicircle with a radius equal to an aircraft'"'"'s worst-case turn radius which lies within zone 3 and which passes through the holding pattern control point tangential to the holding pattern inbound leg.

10. The method of claim 1 wherein the step of providing a predetermined entry maneuver for the selected entry zone comprises automatic commands to an autopilot.

11. The method of claim 1 wherein the step of providing a predetermined entry maneuver for the selected entry zone comprises a manual command displayed to a crew.

12. The method of claim 4 wherein the step of turning to capture the outbound leg of the holding pattern comprises initiating the turn before intersecting the outbound leg.

13. The method of claim 1 wherein the holding pattern comprises a refueling rendezvous orbit.

14. A method for maneuvering an aircraft for entering into a holding pattern, the aircraft position being known and the location and orientation of the holding pattern being known, the method comprising the steps of:

determining a relative bearing between a line from the aircraft to a control point of the holding pattern and an inbound leg line through the control point of the holding pattern;

dividing an airspace around the holding pattern into at least three entry zones, the three entry zones comprising;

a first zone comprising the relative bearing of an angle between −

180 degrees to <

0 degrees;

a second zone comprising the relative bearing of an angle between >

+90 degrees to <

+180 degrees, wherein second zone further comprises;

zone 2b comprising a portion of second zone that lies between the inbound leg and an outbound leg extended; and

zone 2a comprising a remaining portion of the second zone not within zone 2b;

and

a third zone comprising the relative bearing of an angle between 0 to +90 degrees;

providing a preselected entry maneuver for each entry zone,

wherein the entry maneuver for the first zone comprises flying over the control point and capturing the outbound leg of the holding pattern;

the entry maneuver for 2a comprises initially flying toward the control point and turning to capture the outbound leg of the holding pattern;

the entry maneuver for zone 2b comprises initially flying toward the control point and initiating a turn to capture the outbound leg of the holding pattern at a distance from the control point equal to twice an aircraft'"'"'s worst case turning radius; and

the entry maneuver for zone 3 comprises flying to intersect tangentially semicircle with a radius equal to an aircraft'"'"'s worst-case turn radius which lies within zone 3 and which passes through the holding pattern control point tangential to the holding pattern inbound leg;

selecting an entry zone base on the determined relative bearing; and

executing the preselected maneuver for the selected entry zone.