Airborne separation assurance system and required time of arrival function cooperation

Patent metadata

Field	Value
Publication number	US-9761148-B2
Application number	US-84963710-A
Country	US
Kind code	B2
Filing date	Aug 3, 2010
Priority date	Aug 3, 2010
Publication date	Sep 12, 2017
Grant date	Sep 12, 2017

Abstract

Methods and systems are provided for enhancing the functionality of an airborne separation assurance system (ASAS) by modifying it to cooperate with a required time of arrival (RTA) functionality. The system comprises an autopilot configured to execute a trajectory of an aircraft and a flight management system (FMS) in operable communication with the autopilot. The FMS includes a required time of arrival (RTA) system that is configured to determine an RTA aircraft trajectory of the aircraft based on a required time of arrival of the aircraft at a waypoint along the flight plan. The system also includes an airborne separation assurance system (ASAS) in operable communication with the RTA and is configured to determine a spacing trajectory based on a spacing interval from a first reference aircraft.

First claim

What is claimed is:

1. An onboard system for self-controlling an aircraft traversing a flight plan, comprising:
a required time of arrival (RTA) system configured to compile an RTA trajectory based at least upon an RTA at a waypoint of a flight plan of the aircraft and to;
an autopilot in operable communication with the RTA system, the autopilot configured to execute the RTA trajectory that was compiled by the RTA system;
an airborne separation assurance system (ASAS) in operable communication with the RTA and the autopilot and configured to compile a spacing trajectory based at least in part on a spacing interval requirement and determine if the RTA trajectory actually violated the spacing interval requirement, wherein:
when the RTA trajectory has not actually violated the spacing interval requirement then the autopilot continues to execute the RTA trajectory,
when the RTA trajectory has actually violated the spacing interval requirement, then the autopilot executes the spacing trajectory,
the ASAS is further configured to determine if the spacing interval requirement has been re-established by executing the spacing trajectory, and
when the spacing trajectory has re-established the spacing interval requirement, then RTA system is further configured to determine a new RTA trajectory to the waypoint and supply the new RTA trajectory to the autopilot for execution thereby.

2. The onboard system of claim 1 , wherein the ASAS builds the spacing trajectory based at least in part on a communication from an air traffic control authority containing a spacing interval requirement.

3. The onboard system of claim 1 , further comprising a flight deck interface device in operable communication with the ASAS configured to visually provide maneuvering data to a pilot in regard to either the spacing trajectory, the RTA trajectory or both the spacing trajectory and the RTA trajectory.

4. A method for self-controlling an aircraft, comprising the steps of:
executing a required time of arrival (RTA) trajectory by an autopilot that was compiled by a processor based at least upon a required time of arrival at a waypoint of a flight plan of an aircraft;
compiling a spacing trajectory by an airborne separation assurance system based at least in part upon a spacing interval requirement;
determining if the RTA trajectory actually violated the spacing interval requirement;
when the RTA trajectory has not actually violated the spacing interval requirement then continuing the RTA trajectory;
when the RTA trajectory has actually violated the spacing interval requirement, then executing the spacing trajectory;
determining if the spacing interval requirement has been re-established by executing the spacing trajectory; and
when the spacing trajectory has re-established the spacing interval requirement, then determining and executing a new RTA trajectory to the waypoint.

5. The method of claim 4 , wherein the spacing interval requirement is received from an air traffic control authority via one of a data uplink communication and a voice communication.

6. The method of claim 4 , further comprising:
determining if the spacing trajectory has reestablished the spacing interval requirement;
when the spacing trajectory has not actually reestablished the spacing interval requirement, then continue executing the spacing trajectory, otherwise determining a first new RTA trajectory and executing the new RTA trajectory.

7. The method of claim 6 , further comprising updating and recompiling the spacing trajectory if the spacing trajectory.

8. The method of claim 6 , further comprising:
determining if a set of switchback criteria have been satisfied;
when the set of switchback criteria has not been satisfied, then determining and executing the first new RTA trajectory; and
when the set of switchback criteria has been met, then determining and executing a second new RTA trajectory.

Assignees

• Polansky Michal
• Marche Stephane
• Jackson Mike
• Haissig Christine Marie
• Honeywell Int Inc

Inventors

• Polansky Michal
• Marche Stephane
• Jackson Mike
• Haissig Christine Marie

Classifications

• G08G5/0078 Primary

  Physics · mapped topic

• G08G5/045

  Physics · mapped topic

• G08G5/80

  Anti-collision systems · CPC title

• G08G5/723 Primary

  from the aircraft · CPC title