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.

Patent No.:

US 9146557 B1

PDF
Full Text
Expired
Date of Patent:
Sep. 29, 2015

Filed:

Apr. 23, 2014
Applicant:

King Fahd University of Petroleum and Minerals, Dhahran, SA;

Inventors:

Ghufran Ahmed, Dammam, SA;

Sami El Ferik, Dhahran, SA;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 19/00 (2006.01); B64C 17/00 (2006.01); B64B 1/20 (2006.01); G05D 1/08 (2006.01); G05D 1/10 (2006.01); G05D 1/00 (2006.01); B64D 9/00 (2006.01); B64C 39/02 (2006.01); B64D 1/22 (2006.01);
U.S. Cl.
CPC ...
G05D 1/00 (2013.01); B64C 19/00 (2013.01); B64C 39/024 (2013.01); B64D 9/00 (2013.01); G05D 1/08 (2013.01); G05D 1/085 (2013.01); G05D 1/0808 (2013.01); G05D 1/0816 (2013.01); G05D 1/0825 (2013.01); G05D 1/10 (2013.01); G05D 1/101 (2013.01); B64C 17/00 (2013.01); B64C 2201/00 (2013.01); B64C 2201/128 (2013.01); B64C 2201/14 (2013.01); B64D 1/22 (2013.01);
Abstract

The adaptive control method for an unmanned vehicle with a slung load utilizes a feedback linearization controller (FLC) to perform vertical take off, hovering and landing of an unmanned aerial vehicle with a slung load, such as a quadrotor drone or the like. The controller includes a double loop architecture, where the overall controller includes an inner loop having an inner controller which is responsible for controlling the attitude angles and the altitude, and an outer loop having an outer controller responsible for providing the inner loop inner controller with the desired angle values. States, such as including roll, pitch, yaw and/or altitude, are selected as outputs and the feedback linearization technique is used.


Find Patent Forward Citations

Ahmed, Ghufran. (2015). Adaptive control method for unmanned vehicle with slung load (U.S. Patent No. 9146557). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/9146557

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