Works matching DE "SPACE vehicle attitude control systems"

Results: 41

Experimental study and modeling of the deployment process of a spool-first deployable boom.

Published in:

Nonlinear Dynamics, 2025, v. 113, n. 16, p. 20959, doi. 10.1007/s11071-025-11217-w

By:

Kukuryka, Mateusz;
Barciński, Tomasz;
Jarzębowska, Elżbieta

Publication type:

Article

Finite-time output feedback attitude stabilisation for rigid spacecraft with input constraints.

Published in:

IET Control Theory & Applications (Wiley-Blackwell), 2016, v. 10, n. 14, p. 1740, doi. 10.1049/iet-cta.2015.1174

By:

Shihao Sun;
Lin Zhao;
Yingmin Jia

Publication type:

Article

Spacecraft chaotic attitude control with certain actuator failure based on integral sliding mode.

Published in:

Journal of Engineering Research (2307-1877), 2018, v. 6, n. 1, p. 153

By:

Chuang Liu;
Keke Shi;
Zhaowei Sun

Publication type:

Article

Distributed attitude synchronization control for multiple flexible spacecraft without modal variable measurement.

Published in:

International Journal of Robust & Nonlinear Control, 2018, v. 28, n. 10, p. 3435, doi. 10.1002/rnc.4092

By:

Wang, Qishao;
Duan, Zhisheng;
Lv, Yuezu

Publication type:

Article

Robust adaptive fixed-time tracking control of 6-DOF spacecraft fly-around mission for noncooperative target.

Published in:

International Journal of Robust & Nonlinear Control, 2018, v. 28, n. 6, p. 2598, doi. 10.1002/rnc.4038

By:

Huang, Yi;
Jia, Yingmin

Publication type:

Article

A simple saturated control framework for spacecraft with bounded disturbances.

Published in:

International Journal of Robust & Nonlinear Control, 2016, v. 26, n. 3, p. 367, doi. 10.1002/rnc.3303

By:

Jinchang, Hu;
Honghua, Zhang

Publication type:

Article

Adaptive finite-time attitude stabilization for rigid spacecraft with actuator faults and saturation constraints.

Published in:

International Journal of Robust & Nonlinear Control, 2016, v. 26, n. 1, p. 28, doi. 10.1002/rnc.3289

By:

Lu, Kunfeng;
Xia, Yuanqing;
Fu, Mengyin;
Yu, Chunmei

Publication type:

Article

Attitude tracking of rigid spacecraft subject to disturbances of unknown frequencies.

Published in:

International Journal of Robust & Nonlinear Control, 2014, v. 24, n. 16, p. 2231, doi. 10.1002/rnc.2983

By:

Chen, Zhiyong;
Huang, Jie

Publication type:

Article

Hybrid spacecraft attitude control system.

Published in:

International Journal of Multiphysics, 2007, v. 1, n. 2, p. 221, doi. 10.1260/175095407781421586

By:

Varatharajoo, Renuganth;
Ajir, Ramly;
Ahmad, Tamizi

Publication type:

Article

759. Feasibility and principle analyses of morphing airfoil used to control flight attitude.

Published in:

Journal of Vibroengineering, 2012, v. 14, n. 1, p. 388

By:

Du Sha;
Hai-Song Ang;
Long Liu

Publication type:

Article

Constrained large angle reorientation manoeuvres of a space telescope using potential functions and a variable control gain.

Published in:

Aeronautical Journal, 2013, v. 117, n. 1194, p. 807, doi. 10.1017/S0001924000008460

By:

Mengali, G.;
Quarta, A. A.

Publication type:

Article

Spacecraft control with constrained fast reorientation and accurate pointing.

Published in:

Aeronautical Journal, 2004, v. 108, n. 1080, p. 85, doi. 10.1017/S0001924000005030

By:

Mengali, G.;
Quarta, A. A.

Publication type:

Article

On the attitude stabilization of a rigid spacecraft using two skew control moment gyros.

Published in:

Nonlinear Dynamics, 2015, v. 79, n. 3, p. 2079, doi. 10.1007/s11071-014-1796-0

By:

Gui, Haichao;
Jin, Lei;
Xu, Shijie;
Zhang, Jun

Publication type:

Article

A robust attitude control strategy with guaranteed transient performance via modified Lyapunov-based control and integral sliding mode control.

Published in:

Nonlinear Dynamics, 2014, v. 78, n. 3, p. 2205, doi. 10.1007/s11071-014-1598-4

By:

Chen, Zhen;
Cong, Bing;
Liu, Xiang

Publication type:

Article

Attitude stability of a dual-spin spacecraft on a stationary orbit around an asteroid subjected to gravity gradient torque.

Published in:

Astrophysics & Space Science, 2015, v. 355, n. 2, p. 203, doi. 10.1007/s10509-014-2145-y

By:

Zhang, Ming-Jiang;
Zhao, Chang-Yin

Publication type:

Article

Attitude stability of a spacecraft with two flexible solar arrays on a stationary orbit around an asteroid subjected to gravity gradient torque.

Published in:

Astrophysics & Space Science, 2014, v. 351, n. 2, p. 507, doi. 10.1007/s10509-014-1863-5

By:

Zhang, Ming-Jiang;
Zhao, Chang-Yin

Publication type:

Article

A Robust Optimization Approach for Magnetic Spacecraft Attitude Stabilization.

Published in:

Journal of Optimization Theory & Applications, 2017, v. 173, n. 3, p. 994, doi. 10.1007/s10957-016-1035-6

By:

Bruni, Renato;
Celani, Fabio

Publication type:

Article

Finite-Time Stabilization Control for a Rigid Spacecraft under Parameter Uncertainties.

Published in:

Journal of Applied Mathematics, 2014, p. 1, doi. 10.1155/2014/816580

By:

Aihua Zhang;
Jianfei Ni;
Xing Huo

Publication type:

Article

Modeling the angular motion dynamics of spacecraft with a magnetic attitude control system based on experimental studies and dynamic similarity.

Published in:

Doklady Physics, 2017, v. 62, n. 12, p. 543, doi. 10.1134/S1028335817120011

By:

Kulkov, V.;
Medvedskii, A.;
Terentyev, V.;
Firsyuk, S.;
Shemyakov, A.

Publication type:

Article

Anti-disturbance inverse optimal control for spacecraft position and attitude maneuvers with input saturation.

Published in:

Advances in Mechanical Engineering (Sage Publications Inc.), 2016, v. 8, n. 5, p. 1, doi. 10.1177/1687814016649887

By:

Chutiphon Pukdeboon

Publication type:

Article

Attitude Determination and Control System for the PROCYON Micro-Spacecraft.

Published in:

Transactions of the Japan Society of Aeronautical & Space Science, 2017, v. 60, n. 3, p. 181, doi. 10.2322/tjsass.60.181

By:

Satoshi IKARI;
Takaya INAMORI;
Takahiro ITO;
Kaito ARIU;
Kenshiro OGURI;
Masataka FUJIMOTO;
Shinichiro SAKAI;
Yasuhiro KAWAKATSU;
Ryu FUNASE

Publication type:

Article

Electrodynamic control for spacecraft attitude stability in the geomagnetic field.

Published in:

Cosmic Research, 2014, v. 52, n. 6, p. 472, doi. 10.1134/S001095251406001X

By:

Antipov, K.;
Tikhonov, A.

Publication type:

Article

Sensor fault accommodation for the attitude control system of near space vehicle based on T-S fuzzy modeling approach.

Published in:

Journal of Hebei University of Science & Technology, 2013, v. 34, n. 6, p. 552, doi. 10.7535/hbkd.2013yx06011

By:

GAO Zhifeng;
WANG Jufang;
YU Changlong;
QIU Jiqing

Publication type:

Article

A Markley Variables-based Attitude Estimation Method Using Optical Flow and a Star Vector for Spinning Spacecraft.

Published in:

Journal of Navigation, 2018, v. 71, n. 6, p. 1589, doi. 10.1017/S0373463318000516

By:

Ning, Xiaolin;
Ding, Zonghe;
Xu, Mingzhu;
Fang, Jiancheng;
Liu, Gang

Publication type:

Article

Using extended Kalman filter and least squares method for spacecraft attitude estimation.

Published in:

Mathematics in Engineering, Science & Aerospace (MESA), 2011, v. 2, n. 4, p. 445

By:

Veloso Garcia, Roberta;
Koiti Kuga, Hélio;
Zanardi, Maria Cecilia F. P. S.

Publication type:

Article

Shorter Path Design and Control for an Underactuated Satellite.

Published in:

International Journal of Aerospace Engineering, 2017, p. 1, doi. 10.1155/2017/8536732

By:

Lee, Jung-Hyung;
Kim, Donghoon;
Kim, Jichul;
Oh, Hwa-Suk

Publication type:

Article

A Bayesian Classifier for X-Ray Pulsars Recognition.

Published in:

International Journal of Aerospace Engineering, 2016, p. 1, doi. 10.1155/2016/1746925

By:

Liang, Hao;
Zhan, Yafeng;
Duan, Chaowei

Publication type:

Article

Star Image Prediction and Restoration under Dynamic Conditions.

Published in:

Sensors (14248220), 2019, v. 19, n. 8, p. 1890, doi. 10.3390/s19081890

By:

Liu, Di;
Chen, Xiyuan;
Liu, Xiao;
Shi, Chunfeng

Publication type:

Article

Design and Simulation of a MEMS Control Moment Gyroscope for the Sub-Kilogram Spacecraft.

Published in:

Sensors (14248220), 2010, v. 10, n. 4, p. 4130, doi. 10.3390/s100404130

By:

Honglong Chang;
Wenlong Jiao;
Qianyan Fu;
Jianbing Xie;
Weizheng Yuan

Publication type:

Article

Density interface topography recovered by inversion of satellite gravity gradiometry observations.

Published in:

Journal of Geodesy, 2017, v. 91, n. 8, p. 881, doi. 10.1007/s00190-016-0993-7

By:

Ramillien, G.

Publication type:

Article

ANALYSIS OF MATRIX ALGORITHM OF ATTITUDE DETERMINATION.

Published in:

Electronics & Control Systems, 2014, v. 4, n. 42, p. 45, doi. 10.18372/1990-5548.42.8810

By:

Ryzhkov, L. M.;
Ozhog, M. V.

Publication type:

Article

COMPARISON OF THE COVARIANCE ANALYSIS RESULTS OF THE QUEST AND THE TRIAD METHODS.

Published in:

Electronics & Control Systems, 2014, v. 4, n. 42, p. 39, doi. 10.18372/1990-5548.42.8809

By:

Ryzhkov, L. M.;
Stepurenko, D. I.

Publication type:

Article

Optimal nonlinear feedback control of spacecraft rendezvous with finite low thrust between libration orbits.

Published in:

Nonlinear Dynamics, 2014, v. 76, n. 2, p. 1611, doi. 10.1007/s11071-013-1233-9

By:

Peng, Haijun;
Jiang, Xin;
Chen, Biaosong

Publication type:

Article

Optimal Attitude Control for Spacecraft Using Two Variable-Speed Control Moment Gyros.

Published in:

Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 3, p. 371, doi. 10.2322/tastj.17.371

By:

Daiki HIGASHIYAMA;
Katsuhiko YAMADA;
Yasuhiro SHOJI

Publication type:

Article

On Port-Hamiltonian Modeling and Control of Systems with Quaternions.

Published in:

Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 1

By:

Kenji FUJIMOTO;
Tomoya TAKEUCHI;
Yuki MATSUMOTO

Publication type:

Article

Constrained Adaptive Backstepping Control for Re-entry Vehicle.

Published in:

Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 21

By:

Hayato KANEHIRA;
Akio ABE;
Shuichi SASA

Publication type:

Article

Achievement of Long-term On-orbit Operation of the SIMPLE Inflatable Extension Mast.

Published in:

Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 13

By:

Ken HIGUCHI;
Hiroshi FURUYA;
Yasuyuki MIYAZAKI;
Takahira AOKI;
Choji YOSHIDA;
Akihito WATANABE;
Kazuki WATANABE

Publication type:

Article

Spacecraft Attitude Control with RWs via LPV Control Theory: Comparison of Two Different Methods in One Framework.

Published in:

Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 15

By:

Takahiro SASAKI;
Takashi SHIMOMURA;
Sayaka KANATA

Publication type:

Article

Spacecraft Attitude Control Using a Control Moment Gyro with Multiple Degrees of Freedom.

Published in:

Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 75

By:

Hiroki IMANISHI;
Katsuhiko YAMADA;
Yasuhiro SHOJI

Publication type:

Article

Design and Implementation of a Thermopile-Based Earth Sensor.

Published in:

Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 77

By:

Toshinori KUWAHARA;
Kazufumi FUKUDA;
Nobuo SUGIMURA;
Yuji SAKAMOTO;
Kazuya YOSHIDA;
DORSA, Arianna;
PAGANI, Pietro;
BERNELLI, Franco Z.

Publication type:

Article

New Chattering Attenuation Sliding Mode Control of a Flexible Spacecraft.

Published in:

Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 71

By:

Hamidreza NEMATI;
Shinji HOKAMOTO

Publication type:

Article