Follow-me system for unmanned aircraft vehicles

Patent metadata

Field	Value
Publication number	US-9754498-B2
Application number	US-201514846602-A
Country	US
Kind code	B2
Filing date	Sep 4, 2015
Priority date	Sep 5, 2014
Publication date	Sep 5, 2017
Grant date	Sep 5, 2017

Abstract

A system for navigating an aircraft includes a first aircraft with a first communication unit and a second aircraft with a second communication unit. The first aircraft is adapted for determining coordinates of a position of a waypoint. The first communication unit is adapted to transmit the coordinates of the position of the waypoint to the second communication unit. The second aircraft is adapted to navigate to the position of the waypoint. Several waypoints can be provided in this manner such that a flight trajectory is established along which the second aircraft may follow the first aircraft. In addition, the second aircraft may be adapted to follow the first aircraft based on a received identification signal. In certain embodiments, the system can be used such that the second aircraft can follow the first aircraft in case of a failure of systems of the second aircraft.

First claim

What is claimed is:

1. A system for navigating an aircraft, comprising:
a first aircraft with a first communication unit; and
a second aircraft with a second communication unit,
wherein the first aircraft is adapted to determine coordinates of a position of a waypoint,
wherein the first communication unit is adapted to transmit the coordinates of the position of the waypoint to the second communication unit, and
wherein the second aircraft is adapted to navigate to the position of the waypoint,

the first aircraft further comprising:
a first processing unit,
wherein the first processing unit is adapted to determine a position of the second aircraft based on a signal sent from the second communication unit to the first communication unit.

2. The system according to claim 1 ,
wherein the first aircraft is a manned aircraft.

3. The system according to claim 1 ,
wherein the second aircraft is an unmanned aircraft.

4. The system according to claim 1 ,
wherein the first aircraft is adapted to determine coordinates of positions of a plurality of waypoints, which waypoints are determined with respect to a reference system, and
wherein each of the plurality of waypoints together defines a flight trajectory of the first aircraft.

5. The system according to claim 3 ,
wherein the first aircraft is adapted to determine a time value for each of the plurality of waypoints.

6. The system according to claim 3 ,
wherein the second aircraft is adapted to follow the flight trajectory of the first aircraft during flight operation of the first aircraft and the second aircraft.

7. The system according to claim 1 ,
wherein the first processing unit is adapted to determine operating data of the second aircraft, which is selected from the group comprising load factor, speed and altitude.

8. The system according to claim 7 , the first aircraft further comprising:
a display;
wherein the display is adapted to display at least the operating data of the second aircraft.

9. The system according to claim 1 ,
wherein the position of the second aircraft is determined with respect to an Earth reference system.

10. The system according to claim 1 ,
wherein the signal sent from the second communication unit to the first communication unit is a beacon signal, which comprises information about the identity of the second aircraft.

11. The system according to claim 1 ,
wherein the first communication unit comprises a radar, which is adapted to receive a beacon signal sent from the second communication unit in a passive mode such that an angular position of the second aircraft with respect to the first aircraft can be determined.

12. The system according to claim 1 ,
wherein the first communication unit comprises a radar, which is adapted to receive a skin echo from the second aircraft in an active mode such that a range between the first aircraft and the second aircraft can be determined.

13. A method for navigating an aircraft, comprising the steps:
determining coordinates of a position of a waypoint by a first aircraft;
transmitting the coordinates of the position of the waypoint from a first communication unit of the first aircraft to a second communication unit of a second aircraft;
navigating the second aircraft to the position of the waypoint; and
determining a position of the second aircraft based on a signal sent from the second communication unit to a first communication unit of the first aircraft.

Assignees

• Airbus Defence & Space Gmbh

Inventors

• Bousquet Joy
• Vitte Thomas

Classifications

• G08G5/0052

  Physics · mapped topic

• G08G5/0008

  Physics · mapped topic

• G08G5/0047 Primary

  Physics · mapped topic

• G08G5/0056

  Physics · mapped topic

• G05D1/104 Primary

  involving a plurality of aircrafts, e.g. formation flying (traffic control systems for aircraft G08G5/00) · CPC title