Submitting Campus

Daytona Beach

Department

Aerospace Engineering

Document Type

Patent

Publication/Presentation Date

4-18-2017

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 9,625,913 B2

Date of Patent

4-18-2017

Assignee

Embry-Riddle Aeronautical University

Application Number

14/963,827

Date Filed

12-9-2015

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