搜索页_+Spacecraft+angular+rate

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在“Elsevier电子期刊”中，命中：42条，耗时：0.0889559 秒

在所有数据库中总计命中：65条

1.Attitude recovery from feature tracking for estimating angular rate of non-cooperative spacecraft

作者：G. Biondi ; ^{gabriele.biondi@polito.it" class="auth_mail" title="E-mail the corresponding author} ; S. Mauro ; T. Mohtar ; S. Pastorelli ; M. Sorli

关键词：Space debris ; Stereo-vision ; Basis pursuit denoising ; State estimation ; Signal recovery

刊名：Mechanical Systems and Signal Processing

出版年：2017

2.Attitude independent Spacecraft Angular Rate Estimation and Rate Damping using Magnetometer data

作者：Shubha Kapoor^&lowast ; ; ^{shubhak@isac.gov.in" class="auth_mail" title="E-mail the corresponding author} ; Kanu Priya Govila^&lowast ; &lowast ; ; ^{kanug@isac.gov.in" class="auth_mail" title="E-mail the corresponding author} ; M.S. Siva^&lowast ; &lowast ; &lowast ; ; ^{mssiva@isac.gov.in" class="auth_mail" title="E-mail the corresponding author} ; A.K. Kulkarni^&lowast ; &lowast ; &lowast ; &lowast ; ; ^{akkul@isac.gov.in" class="auth_mail" title="E-mail the corresponding author} ; N.K. Philip^&lowast ; &lowast ; &lowast ; &lowast ; ; ^{philip@isac.gov.in" class="auth_mail" title="E-mail the corresponding author}

关键词：Low Earth Orbit ; Kalman Filter ; Spacecraft angular rate ; Three Axis Magnetometer (TAM)

刊名：IFAC-PapersOnLine

出版年：2016

3.Three-Axis Attitude Maneuver of Spacecraft by Reaction Wheels with Rotation Speed Constraints

作者：Shunichiro Nomura^* ; ^{nomura@space.t.u-tokyo.ac.jp" class="auth_mail" title="E-mail the corresponding author} ; Satoshi Ikari^* ; ^{ikari@space.t.u-tokyo.ac.jp" class="auth_mail" title="E-mail the corresponding author} ; Shinichi Nakasuka^* ; ^{nakasuka@space.t.u-tokyo.ac.jp" class="auth_mail" title="E-mail the corresponding author}

关键词：Interplanetary Spacecraft ; Attitude Control ; Reaction Wheels ; Rotation Speed Constraints

刊名：IFAC-PapersOnLine

出版年：2016

4.Gyro-free attitude and rate estimation for a small satellite using SVD and EKF

作者：Chingiz Hajiyev^a ; ^{cingiz@itu.edu.tr" class="auth_mail" title="E-mail the corresponding author} ; Demet Cilden^a ; ^{cilden@itu.edu.tr" class="auth_mail" title="E-mail the corresponding author} ; Yevgeny Somov^b ; ^{e_somov@mail.ru" class="auth_mail" title="E-mail the corresponding author}

关键词：Attitude angles ; Magnetometer ; Sun sensor ; Singular value decomposition ; Extended Kalman filter ; Angular velocity

刊名：Aerospace Science and Technology

出版年：2016

5.The NEOTωIST mission (Near-Earth Object Transfer of angular momentum spin test)

关键词：DSNR ; Detection Signal-to-Noise Ratio ; FoM ; Figure of Merit ; NEO ; Near-Earth Object ; NEOTωIST ; Near-Earth Object Transfer of angular momentum (=ω*I) Spin Test ; LPF ; Lisa Pathfinder Propulsion module

刊名：Acta Astronautica

出版年：2016

6.CMG configuration and Steering Approach for Spacecraft Rapid maneuvers

作者：K Ashok^&lowast ; ; R Aditya^&lowast ; ; Harish K Joglekar^&lowast ; ; MS Siva^&lowast ; &lowast ; ; NK Philip^&lowast ; &lowast ; &lowast ;

关键词：Reorientation Maneuvers ; Agility ; Control Moment Gyros ; High Resolution Imaging

刊名：IFAC-PapersOnLine

出版年：2016

7.Experimental Verification of Attitude Control System for Agile Spacecraft

作者：Andrei Kornienko^* ; ^{andrei.kornienko@airbus.com" class="auth_mail" title="E-mail the corresponding author} ; Jochen Rieber^* ; ^{jochen.rieber@airbus.com" class="auth_mail" title="E-mail the corresponding author} ; Thomas Ott^* ; ^{thomas.ott@airbus.com" class="auth_mail" title="E-mail the corresponding author} ; Ramin Geshnizjani^** ; ^{ramin.geshnizjani@ifr.uni-stuttgart.de" class="auth_mail" title="E-mail the corresponding author} ; Walter Fichter^** ; ^{fichter@ifr.uni-stuttgart.de" class="auth_mail" title="E-mail the corresponding author} ; Jason Forshaw^*** ; ^{j.forshaw@surrey.ac.uk" class="auth_mail" title="E-mail the corresponding author} ; Guglielmo Aglietti^*** ; ^{g.aglietti@surrey.ac.uk" class="auth_mail" title="E-mail the corresponding author}

关键词：Agile Spacecraft ; Attitude Control ; Control Momentum Gyros ; Hardware in the Loop Testbed

刊名：IFAC-PapersOnLine

出版年：2016

8.Robust H_∞ filtering for a spacecraft attitude determination system with affine LPV approach

作者：Shujie Yang ; ^{shujie.yang@buaa.edu.cn" class="auth_mail" title="E-mail the corresponding author} ; Gongliu Yang ; Yuhuan Li ; Jing Li ; Jing Wang

关键词：ADS ; LPV ; Parameter-dependent analysis ; Robust H&infin ; H&infin ; filter ; LMI

刊名：Aerospace Science and Technology

出版年：2016

9.Strong iISS for a class of systems under saturated feedback

作者：Ré ; mi Azouit^a ; ^b ; ^{remi.azouit@l2s.centralesupelec.fr" class="auth_mail" title="E-mail the corresponding author}Author Vitae ; Antoine Chaillet^a ; ^{antoine.chaillet@centralesupelec.fr" class="auth_mail" title="E-mail the corresponding author}Author Vitae ; Yacine Chitour^a ; ^{yacine.chitour@l2s.centralesupelec.fr" class="auth_mail" title="E-mail the corresponding author}Author Vitae ; Luca Greco^a ; ^{luca.greco@l2s.centralesupelec.fr" class="auth_mail" title="E-mail the corresponding author}Author Vitae

关键词：Stability and robustness of nonlinear systems ; Input-to-state stability ; Saturated feedback

刊名：Automatica

出版年：2016

10.Four Reaction Wheels Management: Algorithms Trade-Off and Tuning Drivers for the PROBA-3 Mission

作者：Aymeric Kron^* ; Amé ; lie St-Amour^* ; Jean de Lafontaine^* ; ^{ngc@ngcaerospace.com" class="auth_mail" title="E-mail the corresponding author}

关键词：Spacecraft dynamics ; control ; guidance and navigation

刊名：IFAC-PapersOnLine

出版年：2014

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