Zobrazeno 1 - 10
of 11
pro vyhledávání: '"Akram, Adnane"'
Autor:
Nasri Boualem, Abderrezak, Guessoum, Lotfi, Mostefai, Bensikaddour El habib, Nabil, Hamdadou, Abdelhamid, Ghoul, Akram, Adnane
Publikováno v:
Automatic Control & Computer Sciences; Dec2023, Vol. 57 Issue 6, p563-576, 14p
Autor:
Akram Adnane, Mohammed El-Amine Cheriet, Elhassen Benfriha, Abdellatif Bellar, Mohammed Arezki Si Mohammed, Youssef Kebbati
Publikováno v:
2022 5th International Conference on Advanced Systems and Emergent Technologies (IC_ASET).
Publikováno v:
The Journal of the Astronautical Sciences. 67:1445-1469
This paper investigates a novel adaptive attitude controller design for rigid microsatellite based on feedback linearization approach, in which an accurate attitude pointing is required within a strict power limitation for space environment. The cont
Publikováno v:
Advances in Space Research. 61:1143-1157
Attitude estimation is a critical component of the Attitude Determination and Control System (ADCS) of any satellite. It is used to convert the sensor observation data to an estimated attitude using filtering algorithms. However, in the presence of s
Publikováno v:
2018 2nd IEEE Advanced Information Management,Communicates,Electronic and Automation Control Conference (IMCEC).
A147 estimation is one of the important aspects in Attitude Determination and Control System (ADCS) of a satellite. Under normal working conditions, it is possible to achieve sufficiently a good attitude estimation using regular Kalman filtering. How
Publikováno v:
2016 8th International Conference on Modelling, Identification and Control (ICMIC).
The minimum power consumption is one of the criterion that can be used to choose the best tilt and rotation angles of pyramidal reaction wheel arrangement for attitude control system of microsatellite. In this paper, the simulation results show that
Publikováno v:
2016 UKACC 11th International Conference on Control (CONTROL).
The main goal of this work is to examine the performance analysis of attitude determination and estimation algorithms applied to Low Earth Orbit Satellite in terms of execution time and accuracy. This performance analysis could be useful to the desig
Publikováno v:
Journal of Physics: Conference Series. 783:012020
This paper presents the design of Low Earth Orbit (LEO) micro-satellite attitude controller using reaction wheels, and under actuator faults. Firstly, a backstepping controller is developed when the actuator is fault-free. Then, a fault tolerant cont
Publikováno v:
Journal of Physics: Conference Series. 783:012017
This paper presents a brief synthesis and useful performance analysis of different attitude filtering algorithms (attitude determination algorithms, attitude estimation algorithms, and nonlinear observers) applied to Low Earth Orbit Satellite in term
Publikováno v:
ICMCS
In this paper we propose a method based on mathematical morphology for a building detection of high spatial resolution urban areas satellite images, our method is unsupervised and does not require any additional data except the image itself. It consi