10   Artículos

 
en línea
Jihe Wang, Qingxian Jia and Dan Yu    
The issue of active attitude fault-tolerant stabilization control for spacecrafts subject to actuator faults, inertia uncertainty, and external disturbances is investigated in this paper. To robustly and accurately reconstruct actuator faults, a novel mi... ver más
Revista: Applied Sciences    Formato: Electrónico

 
en línea
Fabio Celani    
The purpose of this paper is to compare performances between stabilization algorithms of quaternion plus attitude rate feedback and rotation matrix plus attitude rate feedback for an Earth-pointing spacecraft with magnetorquers as the only torque actuato... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Yi-Chung Chiu, Loren C. Chang, Chi-Kuang Chao, Tzu-Ya Tai, Kai-Lun Cheng, Hsin-Tzu Liu, Rong Tsai-Lin, Chi-Ting Liao, Wei-Hao Luo, Guan-Po Chiu, Kai-Jie Hou, Ruo-Yu Wang, Glenn Franco Gacal, Pin-An Lin, Sittinat Denduonghatai, Tsai-Ru Yu, Jann-Yenq Liu, Amal Chandran, Kashyapa Bramha Naren Athreyas, Priyadarshan Hari, Joji John Varghese and Mustapha MeftahaddShow full author listremoveHide full author list    
Given the pervasive use of satellite and over the horizon wireless communication technology in modern society, ionospheric disturbances that can disrupt such services are a crucial consideration. Ionospheric irregularities, plasma bubbles and other pheno... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Chih-Chiang Chen and Guan-Shiun Chen    
This paper is concerned with the problem of fixed-time stabilization for a class of uncertain second-order nonlinear systems. By delicately introducing extra manipulations in the feedback domination and revamping the technique of adding a power integrato... ver más
Revista: Applied Sciences    Formato: Electrónico

 
en línea
M. Salim Farissi, Stefano Carletta, Augusto Nascetti and Paolo Teofilatto    
The subject of this work is the implementation and experimental testing of a purely magnetic attitude control strategy, which can provide stabilization after the deployment and pointing of the spacecraft without any attitude information. In particular, t... ver más
Revista: Aerospace    Formato: Electrónico

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