Zobrazeno 1 - 10
of 23
pro vyhledávání: '"N. K. Peyada"'
Autor:
H. O. Verma, N. K. Peyada
Publikováno v:
The Aeronautical Journal. 127:255-267
The aerodynamic modelling is one of the challenging tasks that is generally established using the results of the computational fluid dynamic software and wind tunnel analysis performed either on the scaled model or the prototype. In order to improve
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5098d5449f43da8d4dfb487a5ac90aa0
https://doi.org/10.1017/aer.2022.39
https://doi.org/10.1017/aer.2022.39
Publikováno v:
Journal of the Franklin Institute. 357:13477-13510
This work investigates the semi-global tracking control of a class of uncertain nonlinear systems with input saturation, using adaptive backstepping controller and tuning function design. The control input has been represented as a product of a posit
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f96c76e61aa7a2da26c64cbc3108f539
https://doi.org/10.1016/j.jfranklin.2020.10.003
https://doi.org/10.1016/j.jfranklin.2020.10.003
Autor:
N. K. Peyada, Hari Om Verma
Publikováno v:
The Aeronautical Journal. 125:489-509
The stability and control derivatives are essential parameters in the flight operation of aircraft, and their determination is a routine task using classical parameter estimation methods based on maximum likelihood and least-squares principles. At hi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3e961ae957dfcaa6d3622acce606ee40
https://doi.org/10.1017/aer.2020.95
https://doi.org/10.1017/aer.2020.95
Autor:
N. K. Peyada, Hari Om Verma
Publikováno v:
Aircraft Engineering and Aerospace Technology. 92:895-907
Purpose The purpose of this paper is to investigate the estimation methodology with a highly generalized cost-effective single hidden layer neural network. Design/methodology/approach The aerodynamic parameter estimation is a challenging research are
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9c1d56edb1c1b987a93307cb7bfc6336
https://doi.org/10.1108/aeat-01-2019-0003
https://doi.org/10.1108/aeat-01-2019-0003
Autor:
N. K. Peyada, Hari Om Verma
Publikováno v:
The Aeronautical Journal. 124:271-295
The research paper addresses the problem of estimating aerodynamic parameters using a Gauss-Newton-based optimisation method. The process of the optimisation method lies on the principle of minimising the residual error between the measured and simul
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e33044f3bed4b8de7d7b3cb57a8df4d3
https://doi.org/10.1017/aer.2019.123
https://doi.org/10.1017/aer.2019.123
Autor:
N. K. Peyada, Abhishek Ghosh Roy
Publikováno v:
Aerospace Science and Technology. 71:772-782
In this paper, method of aerodynamic parameter estimation of aircraft, in the presence of process and measurement noise, have been introduced with the help of relevant experiments carried out on simulated as well as real aircraft data. A merger betwe
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c2c0dd804df61bbe7009fa858429cc46
https://doi.org/10.1016/j.ast.2017.10.030
https://doi.org/10.1016/j.ast.2017.10.030
Publikováno v:
Recent Advances in Intelligent Information Systems and Applied Mathematics ISBN: 9783030341510
ICITAM
ICITAM
Aerial robotics is a growing field with tremendous civil and military applications. Potential applications include surveying and maintenance tasks, aerial transportation and manipulation, search and rescue, and surveillance. The challenges associated
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::eca8aa03b3a4ac3433f0f855cee4b55c
https://doi.org/10.1007/978-3-030-34152-7_8
https://doi.org/10.1007/978-3-030-34152-7_8
Publikováno v:
Computational Materials Science. 185:109931
Although Ngo et al. (2006) determined the Young’s modulus and ultimate strength of Ge nanowires experimentally by using atomic force microscopy, orientation dependent these properties, its loading tip velocity dependent mechanical properties were n
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::52dfe5f77b61e4c6c48d5bf6627fbba0
https://doi.org/10.1016/j.commatsci.2020.109931
https://doi.org/10.1016/j.commatsci.2020.109931
Autor:
N. K. Peyada, Abhishek Ghosh Roy
Application of adaptive neuro fuzzy inference system (ANFIS)-based particle swarm optimization (PSO) algorithm to the problem of aerodynamic modeling and optimal parameter estimation for aircraft has been addressed in this chapter. The ANFIS-based PS
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5fade94a9525685aa9ebb3a39efe672e
https://doi.org/10.4018/978-1-5225-5852-1.ch011
https://doi.org/10.4018/978-1-5225-5852-1.ch011
Autor:
N. K. Peyada, S. K. Deb Nath
Publikováno v:
International Journal of Applied Mechanics and Engineering, Vol 20, Iss 4, Pp 733-756 (2015)
In the present study, we have developed a code using Matlab software for solving a rectangular aluminum plate having void, notch, at different boundary conditions discretizing a two dimensional (2D) heat conduction equation by the finite difference t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b35d12fc99a9dd0631fb7bfe5885004a
https://doi.org/10.1515/ijame-2015-0048
https://doi.org/10.1515/ijame-2015-0048