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Dr Dhayalan R

vidwan id: 165447
Male

Assistant Professor, Department of Aerospace Engineering
Indian Institute of Space Science and Technology

Expertise

  • Aerospace Engineering

Publications

Total Articles 8
Books 0
Proceedings 0

Publications

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Scopus

Citations 94
h-index 6

CrossRef

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Citations 70
h-index 5
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Professional Recognition

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Community & Membership

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Aeronautical Society of India

2023
Fellow

Bio

Aerospace system identification, Flight Dynamics, Flight Tests, Aircraft Design, Unmanned Systems, Flight Control.

Personal Details

  • Male
  • Assistant Professor , Indian Institute of Space Science and Technology
  • Indian Institute of Space Science and Technology
PhD
Indian Institute of Technology Kanpur 2015
Assistant Professor Sep 2017 – Present
Indian Institute of Space Science and Technology | Department of Aerospace Engineering
Visiting Faculty Jul 2016 – Nov 2017
Indian Institute of Space Science and Technology

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Co-Authors (1)

Subrahmanyam

Dr Subrahmanyam Saderla

Indian Institute of Technology Kanpur

Scholarly Work

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Scholarly Publications

Aerodynamic and flight dynamic parametric studies of a flapping wing

Open Access
aip

Longitudinal and lateral aerodynamic characterisation of reflex wing Unmanned Aerial Vehicle from flight tests using Maximum Likelihood, Least Square and Neural Gauss Newton methods

Open Access
Article
Authors: Saderla S.;Dhayalan R.;Singh K.;Kumar N.;Ghosh A.K.

Lateral directional parameter estimation of a miniature unmanned aerial vehicle using maximum likelihood and Neural Gauss Newton methods

Open Access
Article

Parameter estimation of UAV from flight data using neural network

Open Access
Article

Non-linear aerodynamic modelling of unmanned cropped delta configuration from experimental data

Open Access
Article

Parameter estimation from near stall flight data using conventional and neural-based methods

Open Access
Article

Parameter Estimation of Unmanned Flight Vehicle Using Wind Tunnel Testing and Real Flight Data

Open Access
Article

Longitudinal parameter estimation from real flight data of unmanned cropped delta flat plate configuration

Open Access
Article