Title

Pressure Sensor Array Based Nonlinear Robust Pitch Control For Small Or Micro Aerial Vehicle

Keywords

aerospace control; Micro aerial vehicle; nonlinear robust control; pressure sensor array

Abstract

Maintaining stable flight of small unmanned or micro aerial vehicles (SUAVs or MAVs) is complicated by many real world challenges. Inspired by biological systems, in this paper, an innovative pressure distribution based pitch control method is proposed. A nonlinear controller, which is robust to uncertainties and un-modeled dynamics, is designed to achieve accurate pitch control. It is expected that the flight control design utilizing the real-time sensed pressure information will significantly enhance the stability and agility of SUAVs or MAVs. © 2012 AACC American Automatic Control Council).

Publication Date

11-26-2012

Publication Title

Proceedings of the American Control Conference

Number of Pages

1732-1736

Document Type

Article; Proceedings Paper

Personal Identifier

scopus

Socpus ID

84869407129 (Scopus)

Source API URL

https://api.elsevier.com/content/abstract/scopus_id/84869407129

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