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:
Dec. 14, 2021

Filed:

Oct. 18, 2017
Applicant:

Deakin University, Waurn Ponds, AU;

Inventors:

Sui Yang Khoo, Waurn Ponds, AU;

Michael John Norton, Waurn Ponds, AU;

Abbas Zahedi Kouzani, Waurn Ponds, AU;

Assignee:

DEAKIN UNIVERSITY, Waurn Ponds, AU;

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 27/08 (2006.01); B64C 27/20 (2006.01); B64C 27/52 (2006.01); B64C 39/02 (2006.01); G05B 13/04 (2006.01); G05D 1/00 (2006.01); G05D 1/08 (2006.01);
U.S. Cl.
CPC ...
G05D 1/0858 (2013.01); B64C 27/08 (2013.01); B64C 27/20 (2013.01); B64C 27/52 (2013.01); B64C 39/024 (2013.01); G05B 13/04 (2013.01); G05D 1/0088 (2013.01); B64C 2201/027 (2013.01); B64C 2201/162 (2013.01);
Abstract

A method of operating a multicopter comprising a body and n thrusters, each thruster independently actuated to vector thrust angularly relative to the body about at least a first axis, the method comprising modelling dynamics of the multicoptor with a mathematical model comprising coupled, non-linear combinations of thruster variables, decoupling the mathematical model into linear combinations of thruster control variables, sensing at least one characteristic of multicopter dynamics, comparing the sensed data with corresponding target characteristic(s), computing adjustments in thruster control variables for reducing the difference between the sensed data and the target characteristic(s) according to a control algorithm, and actuating each thruster according to the computed thruster control variables to converge the multicopter towards the target characteristic(s), wherein the control algorithm is based on the decoupled mathematical model such that each thruster control variable can be adjusted independently.


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