Works matching Space vehicle control systems

Results: 150

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

New Construction Solutions of Gear Using in Space Vehicle Control Systems.

Published in:

Applied Sciences (2076-3417), 2022, v. 12, n. 23, p. 12285, doi. 10.3390/app122312285

By:

Pacana, Jacek;
Siwiec, Dominika;
Pacana, Andrzej

Publication type:

Article

History of spacecraft control systems.

Published in:

Automation & Remote Control, 2013, v. 74, n. 3, p. 331, doi. 10.1134/S0005117913030016

By:

Legostaev, V.;
Mikrin, E.

Publication type:

Article

Flexspline Deformation Analysis Depending on the Polymer Material Used in the Harmonic Drive Prototype.

Published in:

Technical Gazette / Tehnički Vjesnik, 2024, v. 31, n. 6, p. 2087, doi. 10.17559/TV-20230203000316

By:

PACANA, Jacek;
PACANA, Andrzej

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

Contact Dynamics Analysis for HTV Capturing by SSRMS.

Published in:

Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 9

By:

Akihiko HONDA;
Mitsushige ODA;
Hiroki NAKANISHI;
Satoshi SUZUKI

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

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

Spacecraft Dynamics and Control: an Introduction.

Published in:

2014

By:

Forshaw, Jason

Publication type:

Book Review

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

Parameter estimation using unsteady downwash model from real flight data of Hansa-3 aircraft.

Published in:

Aeronautical Journal, 2011, v. 115, n. 1171, p. 577, doi. 10.1017/S0001924000006217

By:

Kumar, R.;
Ghosh, A. K.

Publication type:

Article

The tau of flight control.

Published in:

Aeronautical Journal, 2011, v. 115, n. 1171, p. 521, doi. 10.1017/S0001924000006187

By:

Padfield, G. D.

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

Reaction wheel fault tolerant control for spacecraft attitude stabilization with finite-time convergence.

Published in:

International Journal of Robust & Nonlinear Control, 2013, v. 23, n. 15, p. 1737, doi. 10.1002/rnc.2924

By:

Hu, Qinglei;
Huo, Xing;
Xiao, Bing

Publication type:

Article

Analysis of Efficiency of Systems for Control of the Thermal Regime of Spacecraft.

Published in:

Chemical & Petroleum Engineering, 2016, v. 51, n. 9/10, p. 714, doi. 10.1007/s10556-016-0110-z

By:

Delkov, A.;
Kishkin, A.;
Lavrov, N.;
Tanasienko, F.

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

Structural Design of 3D Printed Spacecraft - ARTSAT2: DESPATCH.

Published in:

Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 45

By:

Kyohei SAWADA;
Meikan CHIN;
Naoto USAMI;
Motoki KIMURA;
Akihiro KUBOTA

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

Near-Earth Asteroid Deflection Mission Using Coulomb Force Attractor.

Published in:

Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 119

By:

Kouhei YAMAGUCHI;
Hiroshi YAMAKAWA

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

Preparation for an On-Orbit Demonstration of an Electrodynamic Tether on the H-II Transfer Vehicle.

Published in:

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

By:

Yasushi OHKAWA;
Satomi KAWAMOTO;
Teppei OKUMURA;
Kentaro IKI;
Yuuta HORIKAWA;
Kazutaka KAWASHIMA;
Yoshiyuki MIURA;
Moto TAKAI;
Masahito WASHIYA;
Osamu KAWASAKI;
Daisuke TSUJITA;
Toru KASAI;
Hirohiko UEMATSU;
Koichi INOUE

Publication type:

Article

Aerodynamics and Flight Capability of a Supersonic Flight Experiment Vehicle.

Published in:

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

By:

Kazuhide MIZOBATA;
Yoshihiro SUZUKI;
Sakae OOISHI;
Satoshi KONDOH;
Takakage ARAI;
Kazuyuki HIGASHINO

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 Line of Sight Maneuver Control Using Skew-arrayed Two Single-Gimbal Control Moment Gyros.

Published in:

Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 31

By:

Hirohisa KOJIMA;
TRIVAILO, Pavel;
Yasuhiro YOSHIMURA

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

Application of a magnetohydrodynamic element in the control loop of a rotating spacecraft with a spike antenna.

Published in:

Cosmic Research, 2009, v. 47, n. 2, p. 156, doi. 10.1134/S0010952509020075

By:

Nazirov, R. R.;
Rabinovich, B. I.;
Mytarev, A. I.

Publication type:

Article

The Rate of Single Event Upsets in Electronic Circuits onboard Spacecraft.

Published in:

Cosmic Research, 2005, v. 43, n. 6, p. 423, doi. 10.1007/s10604-005-0066-9

By:

Kuznetsov, N.

Publication type:

Article

Approximate Calculation of Required and Available Lateral Range Achieved in a Spacecraft Descent to a Preset Point on the Earth's Surface.

Published in:

Cosmic Research, 2005, v. 43, n. 6, p. 442, doi. 10.1007/s10604-005-0068-7

By:

Yaroshevsky, V.

Publication type:

Article

An Effective Algorithm of Aerodynamic Control over Spacecraft Descent.

Published in:

Cosmic Research, 2005, v. 43, n. 6, p. 450, doi. 10.1007/s10604-005-0069-6

By:

Shcherban', I.

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

Investigation and Optimization of Disk-Laser Welding of 1 mm Thick Ti-6Al-4V Titanium Alloy Sheets.

Published in:

Advances in Mechanical Engineering (Sage Publications Inc.), 2015, v. 7, n. 1, p. 1, doi. 10.1155/2014/373561

By:

Caiazzo, Fabrizia;
Alfieri, Vittorio;
Fierro, Ilaria;
Sergi, Vincenzo

Publication type:

Article

In-orbit attitude actuation using solar panels.

Published in:

International Journal of Multiphysics, 2008, v. 2, n. 2, p. 147, doi. 10.1260/175095408785416956

By:

Varatharajoo, Renuganth;
Tan Mei San

Publication type:

Article

Fault Tolerant Control for Near Space Vehicles with Input Saturation Using Disturbance Observer and Neural Networks.

Published in:

Circuits, Systems & Signal Processing, 2015, v. 34, n. 7, p. 2091, doi. 10.1007/s00034-014-9939-6

By:

Yu, Jing;
Chen, Mou

Publication type:

Article

Passive Fault-Tolerant Control Design for Near-Space Hypersonic Vehicle Dynamical System.

Published in:

Circuits, Systems & Signal Processing, 2012, v. 31, n. 2, p. 565, doi. 10.1007/s00034-011-9385-7

By:

Gao, Zhifeng;
Jiang, Bin;
Shi, Peng;
Liu, Jianye;
Xu, Yufei

Publication type:

Article

Multi⁃spacecraft Intelligent Orbit Phasing Control Considering Collision Avoidance.

Published in:

Transactions of Nanjing University of Aeronautics & Astronautics, 2022, v. 39, n. 4, p. 379, doi. 10.16356/j.1005-1120.2022.04.001

By:

LI Jian;
ZHANG Gang

Publication type:

Article

Robust Adaptive Attitude Maneuvering and Vibration Reducing Control of Flexible Spacecraft with Prescribed Performance.

Published in:

Transactions of Nanjing University of Aeronautics & Astronautics, 2019, v. 36, n. 2, p. 214, doi. 10.16356/j.1005-1120.2019.02.004

By:

TAO Jiawei;
ZHANG Tao

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

ANALYSIS OF THE EFFECT OF SOFT SOIL'S PARAMETERS CHANGE ON PLANETARY VEHICLES' DYNAMIC RESPONSE.

Published in:

Journal of Automation, Mobile Robotics & Intelligent Systems, 2017, v. 11, n. 4, p. 65, doi. 10.14313/JAMRIS_4-2017/37

By:

Shibly, Hassan

Publication type:

Article

Robust Adaptive Learning Control for Spacecraft Autonomous Proximity Maneuver.

Published in:

International Journal of Pattern Recognition & Artificial Intelligence, 2017, v. 31, n. 5, p. -1, doi. 10.1142/S0218001417590078

By:

Wu, Shunan;
Wen, Shenghui;
Liu, Yuliang;
Zhang, Kaiming

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

Observer-Based Robust Control for Spacecraft Rendezvous with Thrust Saturation.

Published in:

Abstract & Applied Analysis, 2014, p. 1, doi. 10.1155/2014/710850

By:

Neng Wan;
Ming Liu;
Reza Karimi, Hamid

Publication type:

Article

Investigation of uav systems and flight modes for photogrammetric applications.

Published in:

Photogrammetric Record, 2011, v. 26, n. 136, p. 400, doi. 10.1111/j.1477-9730.2011.00657.x

By:

Eisenbeiss, Henri;
Sauerbier, Martin

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