Modeling and Closed Loop Flight Testing of a Fixed Wing Micro Air Vehicle.

Kandath, Harikumar; Pushpangathan, Jinraj V; Bera, Titas; Dhall, Sidhant; Bhat, M Seetharama

Kandath, Harikumar; Pushpangathan, Jinraj V; Bera, Titas; Dhall, Sidhant; Bhat, M Seetharama.

Afiliación

Kandath H; School of Electrical and Electronic Engineering, Nanyang Technological University, Singapore 639798, Singapore. kharikumar@ntu.edu.sg.
Pushpangathan JV; Department of Aerospace Engineering, Indian Institute of Science, Bengaluru 560012, India. jinrajaero@gmail.com.
Bera T; School of Electrical and Electronic Engineering, Nanyang Technological University, Singapore 639798, Singapore. btitas@ntu.edu.sg.
Dhall S; Department of Aerospace Engineering, Indian Institute of Science, Bengaluru 560012, India. sidhant.dhall@gmail.com.
Bhat MS; Department of Aerospace Engineering, Indian Institute of Science, Bengaluru 560012, India. msbdcl@aero.iisc.ernet.in.

Micromachines (Basel) ; 9(3)2018 Mar 04.

Article en En | MEDLINE | ID: mdl-30424045

Palabras clave

flight testing; lateral dynamics; longitudinal dynamics; micro air vehicle; propeller effects; wind tunnel testing

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Texto completo: 1 Colección: 01-internacional Banco de datos: MEDLINE Idioma: En Revista: Micromachines (Basel) Año: 2018 Tipo del documento: Article País de afiliación: Singapur

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