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:
Mar. 01, 2022

Filed:

Aug. 05, 2019
Applicant:

Wing Aviation Llc, Mountain View, CA (US);

Inventors:

Andre Prager, Sunnyvale, CA (US);

Trevor Shannon, Mountain View, CA (US);

Assignee:

WING AVIATION LLC, Mountain View, CA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 19/00 (2006.01); B64D 1/12 (2006.01); B64D 1/22 (2006.01); B66D 1/48 (2006.01); G05D 1/08 (2006.01); B64C 39/02 (2006.01); B66D 1/12 (2006.01); B66D 1/60 (2006.01); G05D 1/02 (2020.01);
U.S. Cl.
CPC ...
B64C 19/00 (2013.01); B64C 39/024 (2013.01); B64D 1/12 (2013.01); B64D 1/22 (2013.01); B66D 1/12 (2013.01); B66D 1/485 (2013.01); B66D 1/60 (2013.01); G05D 1/0202 (2013.01); G05D 1/0858 (2013.01); B64C 2201/021 (2013.01); B64C 2201/027 (2013.01); B64C 2201/104 (2013.01); B64C 2201/108 (2013.01); B64C 2201/128 (2013.01); B64C 2201/141 (2013.01); B64C 2201/146 (2013.01); B66D 2700/0125 (2013.01); B66D 2700/0141 (2013.01);
Abstract

Described herein are methods and systems to dampen oscillations of a payload coupled to a tether of a winch system arranged on an unmanned aerial vehicle (UAV). For example, the UAV's control system may dampen the oscillations by causing the UAV to switch to a forward flight mode in which movement of the UAV results in drag on the payload, thereby damping the oscillations. In another example, the control system may cause the UAV to reduce an extent flight stabilization along at least one dimension, thereby resulting in damping of the detected oscillations due to energy dissipation during movement of the UAV along the dimension. In this way, the control system could select and carry out one or more such techniques, and could do so during retraction and/or deployment of the tether.


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