A Novel Control Surface for Energy-Optimum Maneuver for Solar-Powered Aircraft

Author:

Dwivedi Vijay Shankar1ORCID,Ghosh A. K.2,Kamath G. M.3ORCID

Affiliation:

1. Research Scholar, Dept. of Aerospace Engineering, Indian Institute of Technology Kanpur, Kanpur, Uttar Pradesh 208016, India; Postdoctoral Research Fellow, School of Aerospace, Transport and Manufacturing, Cranfield Univ., Cranfield, Bedfordshire MK430AL, UK (corresponding author). ORCID: .

2. Professor, Dept. of Aerospace Engineering, Indian Institute of Technology Kanpur, Kanpur, Uttar Pradesh 208016, India.

3. Professor, Dept. of Aerospace Engineering, Indian Institute of Technology Kanpur, Kanpur, Uttar Pradesh 208016, India. ORCID:

Publisher

American Society of Civil Engineers (ASCE)

Subject

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

Reference31 articles.

1. Disturbance observer-based fuzzy control for flexible spacecraft combined attitude & sun tracking system

2. Experimental analysis of a small-scale rotor at various inflow angles;Christopher D. J.;Int. J. Aerosp. Eng.,2018

3. Dwivedi V. S. 2021. “Development of a solar uav using novel design features and optimal energy management techniques.” Ph.D. thesis Dept. of Aerospace Engineering Indian institute of Technology Kanpur.

4. Dwivedi V. S. A. K. Ghosh and G. M. Kamath. 2019. “Design studies to achieve energy optimal attitude for a solar-powered aircraft.” In Proc. 2019 IEEE Aerospace Conf. 1–8. New York: IEEE.

5. Optimal energy utilization for a solar-powered aircraft using sliding-mode-based attitude control;Dwivedi V. S.;IEEE Trans. Aerosp. Electron. Syst.,2021

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