Zobrazeno 1 - 10
of 16
pro vyhledávání: '"Costin Ene"'
Autor:
Teodor-Viorel Chelaru, Cristian Emil Constantinescu, Valentin Pană, Costin Ene, Adrian Chelaru
Publikováno v:
Aerospace, Vol 11, Iss 8, p 660 (2024)
This paper aims to analyze the stability of a special class of single-channel slow-rotating homing missiles using the Frank–Wall stability criterion. To achieve this, starting from the model of a slow-rolling missile with six degrees of freedom (6
Externí odkaz:
https://doaj.org/article/c1b976f8b6d44b8c88283da0b0534dde
Publikováno v:
Aerospace, Vol 9, Iss 9, p 504 (2022)
The paper’s purpose is to present a calculus model for a testing vehicle that can be used to validate guidance, navigation and control systems for reusable launchers in all flight phases. The technical solution is based on a throttleable engine wit
Externí odkaz:
https://doaj.org/article/2bc9ddc6ed5c4727afeb98f0afc7714f
Autor:
Andrei Gradinariu, R. Banici, Bogdan Tatulea, Gerard Mourou, Alexandru Lazar, Veselin Aleksandrov, Andrei Baleanu, Bertrand De Boisdeffre, Daniel Popa, Dmitrii Nistor, Miklos Kiss, Ovidiu Tesileanu, Madalin Rosu, Mihai Caragea, Yoshihide Nakamiya, J. Wheeler, Masruri Masruri, Adrian Toader, Daniel Ursescu, Andrei Naziru, I. Dancus, Loredana Caratas, Vlad Luta, Vicentiu Iancu, Dan Matei, Takahisa Jitsuno, Nicu Stan, Maria Talposi, Gabriel Bleotu, Costin Ene, Mihail Octavian Cernaianu
Publikováno v:
Frontiers in Optics / Laser Science.
Following the completion of the installation and testing of the HPLS 2x10PW laser system at ELI-NP, prospective experiments related to spectral broadening in thin films for post-compression were performed at the HPLS 100TW output.
Autor:
Ioan Dancus, Gabriel V. Cojocaru, Robert Schmelz, Dan Matei, Lidia Vasescu, Dmitrii Nistor, Anda-Maria Talposi, Vicentiu Iancu, Gabriel P. Bleotu, Andrei Naziru, Alexandru Lazar, Alice Dumitru, Antonia Toma, Marius Neagoe, Stefan Popa, Saidbek Norbaev, Cristian Alexe, Andreea Calin, Costin Ene, Adrian Toader, Nicolae Stan, Mihai Caragea, Sorin Moldoveanu, Olivier Chalus, Christophe Derycke, Christophe Radier, Sandrine Ricaud, Vincent Leroux, Caroline Richard, François Lureau, Andrei Baleanu, Romeo Banici, Alexandru Ailincutei, Iulian Moroianu, Andrei Gradinariu, Constantin Caldararu, Cristian Capiteanu, Daniel Ursescu, Domenico Doria, Ovidiu Tesileanu, Takahisa Jitsuno, Razvan Dabu, Kazuo A Tanaka, Sydney Gales, Calin Alexandru Ur
Publikováno v:
EPJ Web of Conferences. 266:13008
We have shown, for the first time in the world, the production of 10 PW peak power laser pulses and their propagation to an experimental area at the Extreme Light Infrastructure - Nuclear Physics (ELI-NP). We are also steadily running the laser syste
Publikováno v:
SCIENTIFIC RESEARCH AND EDUCATION IN THE AIR FORCE. 19:357-364
Publikováno v:
SCIENTIFIC RESEARCH AND EDUCATION IN THE AIR FORCE. 18:185-192
The paper presents an H∞ loop shaping method for the design of the automatic flight control system of an unmanned air vehicle's (UAV's) longitudinal dynamics. The design objectives include robust stabilization with respect to modeling uncertainties
Autor:
Adrian Mihail Stoica, Costin Ene
Publikováno v:
Applied Mechanics and Materials. 841:338-343
Inverting a state-space system A,B,C,D is a problem implying that the transmission zeros, of the system we want to invert, lie in the open left half plane. This is solved by finding an appropriate D matrix. We will show that finding D turns into a st
Autor:
Adrian Mihail Stoica, Costin Ene
Publikováno v:
Applied Mechanics and Materials. 772:418-423
The L1 Adaptive control technique is applied to the F-18 HARV (High Alpha Research Vehicle) aircraft. This control architecture compensates for both the matched and the unmatched uncertainties of the full nonlinear aircraft dynamics. This paper descr
Publikováno v:
MATEC Web of Conferences, Vol 304, p 07008 (2019)
The paper presents a Kalman filtering problem for discrete–time linear systems with parametric uncertainties. A stochastic model with multiplicative noise both in the state and in the output equations is used to represent the system with uncertain
Publikováno v:
IFAC Proceedings Volumes. 46:447-452
An L 1 adaptive controller is proposed to control the short period dynamics of the F-18 HARV experimental aircraft when affected by bounded uncertainties, bounded external disturbance and time delay. The reference model is improved with a linear quad