Dynamics of micro-air-vehicles with flapping wings: A multibody system approach

Roccia, Bruno Antonio et al · Institute of Electrical and Electronics Engineers · 2013

Open-access full text

Quick overview. Review the resource’s basic details, then access the content using the main button. This page shows only the information needed to identify, cite, and open the work.

Author / responsible party

Roccia, Bruno Antonio et al

Publisher

Institute of Electrical and Electronics Engineers

Year

2013

ISSN

1548-0992

ISSN

1548-0992

Language

English

Resource access

Open the content from the main option or choose another available source.

CONICET Digital CONICET Digital OAI-PMH

Entrar por CONICET Digital

Main access

Open-access full text

Texto completo identificado como acceso abierto.

Open text

Summary

Descripción general del contenido del recurso.

This paper presents the development of a dynamic model to study the flight mechanics of a micro-air-vehicle with flapping wings. This model is based on Lagrange's equations for constrained systems. The micro-air-vehicle is modeled as a collection of three rigid bodies a central body and two wings. The wings have prescribed motions relative to the central body, i.e., they are kinematically driven. The numerical integration of all the governing equations, which are differential-algebraic, is performed simultaneously and interactively in the time domain. The integration scheme couples a 4th-order predictor-corrector method, the modified method of Hamming, with a procedure to stabilize the resulting differential-algebraic equations. Fil: Roccia, Bruno Antonio. Consejo Nacional de Investigaciones Científicas y Técnicas. Centro Científico Tecnológico Conicet - Córdoba. Instituto de Estudios Avanzados en Ingeniería y Tecnología. Universidad Nacional de Córdoba. Facultad de Ciencias Exactas Físicas y Naturales. Instituto de Estudios Avanzados en Ingeniería y Tecnología; Argentina Fil: Preidikman, Sergio. Consejo Nacional de Investigaciones Científicas y Técnicas. Centro Científico Tecnológico Conicet - Córdoba. Instituto de Estudios Avanzados en Ingeniería y Tecnología. Universidad Nacional de Córdoba. Facultad de Ciencias Exactas Físicas y Naturales. Instituto de Estudios Avanzados en Ingeniería y Tecnología; Argentina

How to cite

Elegí el formato que necesitás y copiá la referencia al portapapeles.

APA 7

Roccia, B. A. E. A. (2013). Dynamics of micro-air-vehicles with flapping wings: A multibody system approach. http://hdl.handle.net/11336/82250

MLA

Roccia, Bruno Antonio et al. "Dynamics of micro-air-vehicles with flapping wings: A multibody system approach." 2013. http://hdl.handle.net/11336/82250.

Chicago

Roccia, Bruno Antonio et al. 2013. "Dynamics of micro-air-vehicles with flapping wings: A multibody system approach.". http://hdl.handle.net/11336/82250.

Harvard

Roccia, B. A. E. A. 2013, Dynamics of micro-air-vehicles with flapping wings: A multibody system approach, Institute of Electrical and Electronics Engineers, available at: http://hdl.handle.net/11336/82250 [Accessed 5 Aug. 2026].

Share and print

Save the record, copy its permanent link, or print it as a PDF.

Export reference

You can export the record in common formats for use in a reference manager.

RIS BibTeX

Resource details

Bibliographic information to help confirm that this is the correct material.

Title: Dynamics of micro-air-vehicles with flapping wings: A multibody system approach

Author / contributors: Roccia, Bruno Antonio et al

Publisher: Institute of Electrical and Electronics Engineers

Publication year: 2013

ISSN: 1548-0992

ISSN: 1548-0992

Language: English

Subjects

Explore related resources through these subjects.

Multibody Systems; Micro Air Vehicles; Flapping Wings; Mav; https://purl.org/becyt/ford/2.3; https://purl.org/becyt/ford/2