Welcome to the InfoSci Platform
Control of a Wing Type Flat-Plate for an Ornithopter Autonomous Robot With Differential Flatness

Control of a Wing Type Flat-Plate for an Ornithopter Autonomous Robot With Differential Flatness

Elkin Yesid Veslin Díaz, Cesar Francisco Bogado-Martínez, Max Suell Dutra, Luciano Santos Constantin Raptopoulos
Copyright: © 2020 |Pages: 37
ISBN13: 9781799801375|ISBN10: 1799801373|EISBN13: 9781799801382
DOI: 10.4018/978-1-7998-0137-5.ch009
Cite Chapter Cite Chapter

MLA

Díaz, Elkin Yesid Veslin, et al. "Control of a Wing Type Flat-Plate for an Ornithopter Autonomous Robot With Differential Flatness." Handbook of Research on Advanced Mechatronic Systems and Intelligent Robotics, edited by Maki K. Habib, IGI Global, 2020, pp. 209-245. https://doi.org/10.4018/978-1-7998-0137-5.ch009

APA

Díaz, E. Y., Bogado-Martínez, C. F., Dutra, M. S., & Raptopoulos, L. S. (2020). Control of a Wing Type Flat-Plate for an Ornithopter Autonomous Robot With Differential Flatness. In M. Habib (Ed.), Handbook of Research on Advanced Mechatronic Systems and Intelligent Robotics (pp. 209-245). IGI Global. https://doi.org/10.4018/978-1-7998-0137-5.ch009

Chicago

Díaz, Elkin Yesid Veslin, et al. "Control of a Wing Type Flat-Plate for an Ornithopter Autonomous Robot With Differential Flatness." In Handbook of Research on Advanced Mechatronic Systems and Intelligent Robotics, edited by Maki K. Habib, 209-245. Hershey, PA: IGI Global, 2020. https://doi.org/10.4018/978-1-7998-0137-5.ch009

Export Reference

Mendeley
Favorite

Abstract

In this chapter, a two-degree-of-freedom controller that exploits the flat properties of a three degree-of-freedom wing type flat-plate for an Ornithopter Autonomous robot is proposed. A set of kinematical patterns inspired by nature is used to simulate the wing's movement around two wingtip trajectories; also, the effects of the aerodynamical forces as a function of the wind velocity and the wing's angle of attack are considered. In order to control the system, the effects of these forces are viewed as disturbs that affect the wing's dynamics. The proposed control scheme drives the device through the desired path by generating a set of desired inputs which are compensated by a feedback loop when the aerodynamical forces actuate upon the system.

Request Access

You do not own this content. Please login to recommend this title to your institution's librarian or purchase it from the IGI Global bookstore.