Autonomous Flight Test of a Novel Nonconventional Biplane Micro Air Vehicle-Reference-Cited by-同舟云学术

Autonomous Flight Test of a Novel Nonconventional Biplane Micro Air Vehicle

Published:2022-09 Issue:5 Volume:35 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Jana Shuvrangshu¹^ORCID,Shivkumar Shashank²^ORCID,Shewale Mayur³,Kandath Harikumar⁴^ORCID,Ramesh Meghana⁴^ORCID,Balasubramaniam Susheel²^ORCID,Khanapuri Eshaan³,Bhat M. Seetharama⁵

Affiliation:

1. Research Associate, Micro Air Vehicle Laboratory, Dept. of Aerospace Engineering, Indian Institute of Science, Bengaluru, Karnataka 560012, India (corresponding author). ORCID: .

2. Research Assistant, Micro Air Vehicle Laboratory, Dept. of Aerospace Engineering, Indian Institute of Science, Bengaluru, Karnataka 560012, India. ORCID: .

3. Research Assistant, Micro Air Vehicle Laboratory, Dept. of Aerospace Engineering, Indian Institute of Science, Bengaluru, Karnataka 560012, India.

4. Research Associate, Micro Air Vehicle Laboratory, Dept. of Aerospace Engineering, Indian Institute of Science, Bengaluru, Karnataka 560012, India. ORCID: .

5. Professor, Micro Air Vehicle Laboratory, Dept. of Aerospace Engineering, Indian Institute of Science, Bengaluru, Karnataka 560012, India.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

https://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001452

Reference47 articles.

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2. Nonlinear Flight Dynamics and Control of a Fixed-Wing Micro Air Vehicle: Numerical, System Identification and Experimental Investigations

3. Armanini S. F. J. V. Caetano C. C. de Visser G. C. de Croon and M. Mulder. 2016. “Aerodynamic model identification of a clap-and-fling flapping-wing MAV: A comparison between quasi-steady and black-box approaches.” In Proc. AIAA Atmospheric Flight Mechanics Conf. 0014. Reston VA: American Institute of Aeronautics and Astronautics.

4. Armanini S. F. C. C. de Visser and G. de Croon. 2015. “Black-box LTI modelling of flapping-wing micro aerial vehicle dynamics.” In Proc. AIAA Atmospheric Flight Mechanics Conference 0234. Reston VA: American Institute of Aeronautics and Astronautics.

5. Beard, R., and T. McLain. 2009. Navigation, guidance and control of small unmanned aircraft. Princeton, NJ: Princeton University Press.

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