IP Library › Granted Patent US 7,061,401
Granted Patent B2
US 7,061,401 · App. 10/889,449 · Granted Jun 13, 2006

Method and apparatus for detecting a flight obstacle

Assignee: Bodenseewerk Gerätetechnik GmbH
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Quick Facts
Patent No.
US 7,061,401
App. No.
10/889,449
Granted
Jun 13, 2006
Kind
B2
Abstract

An apparatus for and a method of detecting a flight obstacle ( 28, 30, 32, 34 ) in the surroundings ( 50 ) of an aircraft ( 4 ), in particular for collision warning purposes, wherein images of the surroundings ( 50 ) are recorded, the flight obstacle ( 28, 30, 32, 34 ) is detected from the images and provided with an identification, and a signal ( 66, 68, 76 ) associated with the identification is outputted in a ground station ( 6 ). In order to guarantee a high level of certainty in respect to the control of the aircraft ( 4 ) which is effected automatically or by a ground control pilot it is proposed that detection and allocation of the identification are effected on board the aircraft ( 4 ) and the identification is sent to the ground station ( 6 ).

Claims (14)

1. A method of detecting a flight obstacle ( 28 , 30 , 32 , 34 ) in the surroundings ( 50 ) of an unmanned aircraft ( 4 ), wherein at least two images of at least one respective part of the surroundings ( 50 ) are recorded, the flight obstacle ( 28 , 30 , 32 , 34 ) is detected from the images and provided with an identification, and a signal ( 66 , 68 , 76 ) associated with the identification is outputted in a ground station ( 6 ), characterised in that detection and allocation of the identification are effected onboard the aircraft ( 4 ) and the identification is sent to the ground station ( 6 ).

2. A method according to claim 1 characterised in that a classification of a risk potential of the flight obstacle ( 28 , 30 , 32 , 34 ) is effected on board the aircraft ( 4 ) and is sent to the ground station ( 6 ).

3. A method according to claim 1 characterised in that a measurement with respect to the flight obstacle ( 28 , 30 , 32 , 34 ) is effected with an active measurement signal.

4. A method according to claim 1 characterised in that an avoidance trajectory ( 42 ) is ascertained on board and data associated with the avoidance trajectory ( 42 ) are communicated to the ground station ( 6 ).

5. A method according to claim 4 characterised in that the avoidance trajectory ( 42 ) is ascertained with the incorporation of items of information ascertained on board about the surroundings ( 50 ) and/or the flight situation of the aircraft ( 4 ).

6. A method according to claim 4 characterised in that a decision as to whether the aircraft ( 4 ) is to fly on the avoidance trajectory ( 42 ) is made by a control apparatus ( 18 ) on board the aircraft ( 4 ).

7. A method according to claim 1 characterised in that a detail image ( 38 ) representing the flight obstacle ( 28 , 30 ) is sent to and displayed at the ground station ( 6 ).

8. A method according to claim 7 characterised in that a portion of an image used for detection of the flight obstacle ( 28 , 30 ) is used as the detail image ( 38 ).

9. A method according to claim 7 characterised in that the detail image ( 38 ) is recorded in a spectral range which differs from the spectral range of the images used for detection of the flight obstacle ( 28 , 30 , 32 , 34 ).

10. A method according to claim 1 characterised in that the images from which the flight obstacle ( 28 , 30 , 32 , 34 ) is detected are recorded in the infrared spectral range.

11. A method according to claim 1 characterised in that a moving image of the flight obstacle ( 28 , 30 ) is sent to the ground station ( 6 ).

12. An apparatus for detecting a flight obstacle ( 28 , 30 , 32 , 34 ) in the surroundings ( 50 ) of an unmanned aircraft ( 4 ), comprising at least one camera unit ( 24 ) for recording at least a part of the surroundings ( 50 ) and an evaluation apparatus ( 26 ) for detecting the flight obstacle ( 28 , 30 , 32 , 34 ) during the flight and associating an identification with the flight obstacle ( 28 , 30 , 32 , 34 ), characterised in that the evaluation apparatus ( 26 ) is electrically connected to the at least one camera unit ( 24 ) and a transmitting device for sending the identification to a ground station ( 6 ).

13. Apparatus according to claim 12 characterised by a detail image unit for extraction of a detail image ( 38 ) showing the flight obstacle ( 28 , 30 ) and for forwarding the detail image ( 38 ) to the transmitting device.

14. Apparatus according to claim 12 characterised by a first camera unit ( 24 ) for recording an overall image in a first spectral range and a second camera unit ( 36 ) for recording an image, such as a detail image ( 38 ) in a spectral range which is different from the first spectral range.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 12, 2004
From: VOOS, HOLGER; KOCH, RENE; DAHNE, CLAUS; ARNDT, MARTIN; GROSS, MICHAEL
To: BODENSEEWERK GERTETECHNIK GMBH
Reel/Frame 015585/0776 →
Priority Claims (1)
DE 103 36 928 · Aug 7, 2003 · national
Continuity (1)
Related Publication 20050109872A1 · May 26, 2005