The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jun. 11, 2019

Filed:

Sep. 29, 2016
Applicant:

Airbus Defence and Space Gmbh, Taufkirchen, DE;

Inventor:

Manfred Hiebl, Neuburg a. d. Donau, DE;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G05D 1/00 (2006.01); G05D 1/02 (2006.01); G05D 1/10 (2006.01); G08G 5/00 (2006.01); B64C 39/02 (2006.01); G01C 21/00 (2006.01); G08G 5/06 (2006.01); G05D 1/06 (2006.01); H04B 7/155 (2006.01); H04L 29/08 (2006.01);
U.S. Cl.
CPC ...
G08G 5/0069 (2013.01); B64C 39/024 (2013.01); G01C 21/00 (2013.01); G05D 1/0022 (2013.01); G05D 1/0676 (2013.01); G08G 5/003 (2013.01); G08G 5/0013 (2013.01); G08G 5/065 (2013.01); B64C 2201/18 (2013.01); H04B 7/155 (2013.01); H04L 67/12 (2013.01);
Abstract

An unmanned aerial vehicle with lift and propulsion system and a flight control system and method. The flight control system has a flight control unit, a navigation system, a communication system and an actuator system. The flight control unit can calculate, based on data from the navigation system and/or data of a ground control station, control commands which can be fed to the actuator system for actuating the lift and propulsion system. The ground control station is configured to control and/or monitor the aerial vehicle. The aerial vehicle has a monitoring unit to monitor the communication system to determine whether all the communication links are interrupted. The monitoring unit can cause the flight control unit to land the aerial vehicle safely at a suitable landing site based on stored data relating to current flight conditions and nearby landing sites.


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