Document Type

Patent

Publication/Presentation Date

7-21-2016

Abstract/Description

An unmanned aerial vehicle (UAV) is provided with a plural­ity of synthetic jet actuators and a nonlinear robust controller. The controller compensates for uncertainty in a mathematic model that describes the function of the synthetic jet actua­tors. Compensation is provided by the use of constant feed­forward best guess estimates that eliminate the need for more highly computationally burdensome approaches such as the use of time-varying adaptive parameter estimation algo­rithms.

Patent Number

US 2016/0209850 Al

Assignee

Embry-Riddle Aeronautical University

Application Number

14/963,827

Date Filed

12-9-2015

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