Zobrazeno 1 - 8
of 8
pro vyhledávání: '"Appasaheb Malagaudanavar"'
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 234:997-1013
In this paper, we propose a robust nonlinear position and attitude control method for quadrotor using higher order sliding mode control concept. The control of quadrotor is realized in an inner- and outer-loop structure. Both inner- (attitude control
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b8b0043293fb7230e5ed32957c1845c0
https://doi.org/10.1177/0954410019893215
https://doi.org/10.1177/0954410019893215
Publikováno v:
Applied Soft Computing. 121:108721
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3986e87cc92a97e134255f44d76a3ead
https://doi.org/10.1016/j.asoc.2022.108721
https://doi.org/10.1016/j.asoc.2022.108721
Publikováno v:
Lecture Notes in Mechanical Engineering ISBN: 9789811547782
Today, many ageing aircrafts in air forces of many countries are in service beyond their designed total technical and calendar service life. In general, typical military fighter and trainer aircraft airframe structure is designed for a service life o
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::455f628133f7f005290453bf646c1233
https://doi.org/10.1007/978-981-15-4779-9_3
https://doi.org/10.1007/978-981-15-4779-9_3
Publikováno v:
Journal of Intelligent & Fuzzy Systems. 34:3891-3901
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0170974ad7595819af301b313ae41818
https://doi.org/10.3233/jifs-169560
https://doi.org/10.3233/jifs-169560
Publikováno v:
Composite Structures. 185:132-147
The present study aims to minimize the weight of multi-laminate aerospace structures by a classical Genetic Algorithm (GA) interfaced with a CAE solver. The structural weight minimization is a multi-objective optimization problem subjected to fulfill
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d4711b1c5589ec396062c09c0782d532
https://doi.org/10.1016/j.compstruct.2017.10.041
https://doi.org/10.1016/j.compstruct.2017.10.041
Publikováno v:
Computational Intelligence: Theories, Applications and Future Directions-Volume I ISBN: 9789811311314
This paper presents the application of fuzzy logic theory for aerodynamic modeling of the fixed wing aircraft. For the demonstration purpose, yawing moment control and stability derivatives of ATTAS aircraft are extracted from the recorded flight dat
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f4cb6e3f446f3844f195e6a26d153818
https://doi.org/10.1007/978-981-13-1132-1_33
https://doi.org/10.1007/978-981-13-1132-1_33
Publikováno v:
2017 International Conference on Sensing, Diagnostics, Prognostics, and Control (SDPC).
This paper presents an application of fuzzy logic theory for modeling a data driven fuzzy model of Angle of Attack sensor of ATAS aircraft using the recorded linear acceleration, airspeed, pitch angle and elevator deflection data of aircraft as input
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a34555d9ccd15120210c25999db7042f
https://doi.org/10.1109/sdpc.2017.91
https://doi.org/10.1109/sdpc.2017.91
Publikováno v:
2017 International Conference on Sensing, Diagnostics, Prognostics, and Control (SDPC).
In this paper, we present the application of radial basis function (RBF) neural network for aerodynamic parameter estimation. The Two-Stage RBF neural network (NN) architecture is proposed for complete aerodynamic modelling. The RBF NN is trained by
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::77403da52b15e6894fd88cb5c51de7d9
https://doi.org/10.1109/sdpc.2017.93
https://doi.org/10.1109/sdpc.2017.93