FRINK Linked Data Fragments server

Matches in SemOpenAlex for { <https://semopenalex.org/work/W1998465268> ?p ?o ?g. }

• W1998465268 endingPage "1248" @default.
• W1998465268 startingPage "1240" @default.
• W1998465268 abstract "No AccessEngineering NoteBounded Output Feedback of Rigid-Body Attitude via Angular Velocity ObserversJinchang Hu and Honghua ZhangJinchang HuNational Key Laboratory of Science and Technology on Space Intelligent Control, Beijing Institute of Control Engineering, 100190 Beijing, People’s Republic of China*Ph.D. Candidate, National Key Laboratory of Science and Technology on Space Intelligent Control; .Search for more papers by this author and Honghua ZhangNational Key Laboratory of Science and Technology on Space Intelligent Control, Beijing Institute of Control Engineering, 100190 Beijing, People’s Republic of China†Professor, National Key Laboratory of Science and Technology on Space Intelligent Control; .Search for more papers by this authorPublished Online:2 Jul 2013https://doi.org/10.2514/1.57187SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Wen J. T. and Kreutz–Delgado K., “The Attitude Control Problem,” IEEE Transactions on Automatic Control, Vol. 36, No. 10, 1991, pp. 1148–1162. doi:https://doi.org/10.1109/9.90228. IETAA9 0018-9286 CrossrefGoogle Scholar[2] Joshi S. M., Kelkar A. G. and Wen J. T.-Y., “Robust Attitude Stabilization of Spacecraft Using Nonlinear Quaternion Feedback,” IEEE Transactions on Automatic Control, Vol. 40, No. 10, 1995, pp. 1800–1803. doi:https://doi.org/10.1109/9.467669. IETAA9 0018-9286 CrossrefGoogle Scholar[3] Boskovic J. D., Li S.-M. and K. Mehra R., “Robust Adaptive Variable Structure Control of Spacecraft Under Control Input Saturation,” Journal of Guidance, Control, and Dynamics, Vol. 24, No. 1, 2001, pp. 14–22. doi:https://doi.org/10.2514/2.4704. JGCDDT 0162-3192 LinkGoogle Scholar[4] Boskovic J. D., Li S.-M. and Mehra R. K., “Robust Tracking Control Design for Spacecraft Under Control Input Saturation,” Journal of Guidance, Control, and Dynamics, Vol. 27, No. 4, 2004, pp. 627–633. doi:https://doi.org/10.2514/1.1059. JGCDDT 0162-3192 LinkGoogle Scholar[5] Wallsgrove R. J. and Akella M. R., “Globally Stabilizing Saturated Attitude Control in the Presence of Bounded Unknown Disturbances,” Journal of Guidance, Control, and Dynamics, Vol. 28, No. 5, 2005, pp. 957–963. doi:https://doi.org/10.2514/1.9980. JGCDDT 0162-3192 LinkGoogle Scholar[6] Ali I., Radice G. and Kim J., “Backstepping Control Design with Actuator Torque Bound for Spacecraft Attitude Maneuver,” Journal of Guidance, Control, and Dynamics, Vol. 33, No. 1, 2010, pp. 254–259. doi:https://doi.org/10.2514/1.45541. JGCDDT 0162-3192 LinkGoogle Scholar[7] Su Y. and Zheng C., “Globally Asymptotic Stabilization of Spacecraft with Simple Saturated Proportional-Derivative Control,” Journal of Guidance, Control, and Dynamics, Vol. 34, No. 6, 2011, pp. 1932–1935. doi:https://doi.org/10.2514/1.54254. JGCDDT 0162-3192 LinkGoogle Scholar[8] Salcudean S., “A Globally Convergent Angular Velocity Observer for Rigid Body Motion,” IEEE Transactions on Automatic Control, Vol. 36, No. 12, 1991, pp. 1493–1497. doi:https://doi.org/10.1109/9.106169. IETAA9 0018-9286 CrossrefGoogle Scholar[9] Aghannan N. and Rouchon P., “An Intrinsic Observer for a Class of Lagrangian Systems,” IEEE Transactions on Automatic Control, Vol. 48, No. 6, 2003, pp. 936–945. doi:https://doi.org/10.1109/TAC.2003.812778. IETAA9 0018-9286 CrossrefGoogle Scholar[10] Caccavale F. and Villani L., “Output Feedback Control for Attitude Tracking,” Systems and Control Letters, Vol. 38, No. 2, 1999, pp. 91–98. doi:https://doi.org/10.1016/S0167-6911(99)00050-X. SCLEDC 0167-6911 CrossrefGoogle Scholar[11] Lizarralde F. and Wen J. T., “Attitude Control Without Angular Velocity Measurement: A Passivity Approach,” IEEE Transactions on Automatic Control, Vol. 41, No. 3, 1996, pp. 468–472. doi:https://doi.org/10.1109/9.486654. IETAA9 0018-9286 CrossrefGoogle Scholar[12] Tsiotras P., “Further Passivity Results for the Attitude Control Problem,” IEEE Transactions on Automatic Control, Vol. 43, No. 11, 1998, pp. 1597–1600. doi:https://doi.org/10.1109/9.728877. IETAA9 0018-9286 CrossrefGoogle Scholar[13] Akella M. R., Valdivia A. and Kotamraju G. R., “Velocity-Free Attitude Controllers Subject to Actuator Magnitude and Rate Saturations,” Journal of Guidance, Control, and Dynamics, Vol. 28, No. 4, 2005, pp. 659–666. doi:https://doi.org/10.2514/1.8784. JGCDDT 0162-3192 LinkGoogle Scholar[14] Tayebi A., “Unit Quaternion-Based Output Feedback for the Attitude Tracking Problem,” IEEE Transactions on Automatic Control, Vol. 53, No. 6, 2008, pp. 1516–1520. doi:https://doi.org/10.1109/TAC.2008.927789. IETAA9 0018-9286 CrossrefGoogle Scholar[15] Bertrand A., Hamel T., Piet–Lahanier H. and Mahony A., “Attitude Tracking of Rigid Bodies on the Special Orthogonal Group with Bounded Partial State Feedback,” Joint 48th IEEE Conference on Decision and Control and 28th Chinese Control Conference, Shanghai, People’s Republic of China, Dec. 2009, pp. 2972–2977. doi:https://doi.org/10.1109/CDC.2009.5400702 Google Scholar[16] Astolfi A., Ortega R. and Venkatraman A., “A Globally Exponentially Convergent Immersion and Invariance Speed Observer for N Degrees of Freedom Mechanical Systems,” Joint 48th IEEE Conference on Decision and Control and 28th Chinese Control Conference, Shanghai, People’s Republic of China, IEEE Press, Piscataway, NJ, Dec. 2009, pp. 6508–6512. Google Scholar[17] Astolfi A., Ortega R. and Venkatraman A., “A Globally Exponentially Convergent Immersion and Invariance Speed Observer for Mechanical Systems with Non-Holonomic Constraints,” Automatica, Vol. 46, No. 1, 2010, pp. 182–189. doi:https://doi.org/10.1016/j.automatica.2009.10.027 ATCAA9 0005-1098 CrossrefGoogle Scholar[18] Astolfi A., Karagiannis D. and Ortega R., Nonlinear and Adaptive Control with Applications, Springer, New York, NY, 2008, Chaps. 1–5. CrossrefGoogle Scholar[19] Stamnes N., Aamo O. M. and Kaasa G.-O., “A Constructive Speed Observer Design for General Euler–Lagrange Systems,” Automatica, Vol. 47, No. 10, 2011, pp. 2233–2238. doi:https://doi.org/10.1016/j.automatica.2011.08.006 ATCAA9 0005-1098 CrossrefGoogle Scholar[20] Lo S.-C. and Chen Y.-P., “Smooth Sliding-Mode Control for Spacecraft Attitude Tracking Maneuvers,” Journal of Guidance, Control, and Dynamics, Vol. 18, No. 6, 1995, pp. 1345–1349. doi:https://doi.org/10.2514/3.21551. JGCDDT 0162-3192 LinkGoogle Scholar[21] Isidori A., Nonlinear Control Systems II, Springer, New York, NY, 1999, p. 17. CrossrefGoogle Scholar Previous article Next article" @default.
• W1998465268 created "2016-06-24" @default.
• W1998465268 creator A5018876172 @default.
• W1998465268 creator A5038270756 @default.
• W1998465268 date "2013-07-01" @default.
• W1998465268 modified "2023-10-09" @default.
• W1998465268 title "Bounded Output Feedback of Rigid-Body Attitude via Angular Velocity Observers" @default.
• W1998465268 cites W1611538460 @default.
• W1998465268 cites W1974093707 @default.
• W1998465268 cites W1982426990 @default.
• W1998465268 cites W2017195813 @default.
• W1998465268 cites W2046709293 @default.
• W1998465268 cites W2061822593 @default.
• W1998465268 cites W2067067397 @default.
• W1998465268 cites W2077974163 @default.
• W1998465268 cites W2080985978 @default.
• W1998465268 cites W2085962256 @default.
• W1998465268 cites W2097020018 @default.
• W1998465268 cites W2101413622 @default.
• W1998465268 cites W2103095193 @default.
• W1998465268 cites W2110497366 @default.
• W1998465268 cites W2129092695 @default.
• W1998465268 cites W2134858417 @default.
• W1998465268 cites W2137427741 @default.
• W1998465268 cites W2169064059 @default.
• W1998465268 cites W4205940976 @default.
• W1998465268 doi "https://doi.org/10.2514/1.57187" @default.
• W1998465268 hasPublicationYear "2013" @default.
• W1998465268 type Work @default.
• W1998465268 sameAs 1998465268 @default.
• W1998465268 citedByCount "31" @default.
• W1998465268 countsByYear W19984652682014 @default.
• W1998465268 countsByYear W19984652682015 @default.
• W1998465268 countsByYear W19984652682016 @default.
• W1998465268 countsByYear W19984652682017 @default.
• W1998465268 countsByYear W19984652682018 @default.
• W1998465268 countsByYear W19984652682019 @default.
• W1998465268 countsByYear W19984652682020 @default.
• W1998465268 countsByYear W19984652682021 @default.
• W1998465268 countsByYear W19984652682022 @default.
• W1998465268 countsByYear W19984652682023 @default.
• W1998465268 crossrefType "journal-article" @default.
• W1998465268 hasAuthorship W1998465268A5018876172 @default.
• W1998465268 hasAuthorship W1998465268A5038270756 @default.
• W1998465268 hasConcept C121332964 @default.
• W1998465268 hasConcept C127413603 @default.
• W1998465268 hasConcept C133731056 @default.
• W1998465268 hasConcept C134306372 @default.
• W1998465268 hasConcept C146978453 @default.
• W1998465268 hasConcept C154945302 @default.
• W1998465268 hasConcept C155710575 @default.
• W1998465268 hasConcept C17744445 @default.
• W1998465268 hasConcept C191935318 @default.
• W1998465268 hasConcept C199539241 @default.
• W1998465268 hasConcept C200127275 @default.
• W1998465268 hasConcept C2524010 @default.
• W1998465268 hasConcept C26517878 @default.
• W1998465268 hasConcept C2775924081 @default.
• W1998465268 hasConcept C2778304055 @default.
• W1998465268 hasConcept C29829512 @default.
• W1998465268 hasConcept C33923547 @default.
• W1998465268 hasConcept C34388435 @default.
• W1998465268 hasConcept C38652104 @default.
• W1998465268 hasConcept C41008148 @default.
• W1998465268 hasConcept C47446073 @default.
• W1998465268 hasConcept C5594486 @default.
• W1998465268 hasConcept C62520636 @default.
• W1998465268 hasConceptScore W1998465268C121332964 @default.
• W1998465268 hasConceptScore W1998465268C127413603 @default.
• W1998465268 hasConceptScore W1998465268C133731056 @default.
• W1998465268 hasConceptScore W1998465268C134306372 @default.
• W1998465268 hasConceptScore W1998465268C146978453 @default.
• W1998465268 hasConceptScore W1998465268C154945302 @default.
• W1998465268 hasConceptScore W1998465268C155710575 @default.
• W1998465268 hasConceptScore W1998465268C17744445 @default.
• W1998465268 hasConceptScore W1998465268C191935318 @default.
• W1998465268 hasConceptScore W1998465268C199539241 @default.
• W1998465268 hasConceptScore W1998465268C200127275 @default.
• W1998465268 hasConceptScore W1998465268C2524010 @default.
• W1998465268 hasConceptScore W1998465268C26517878 @default.
• W1998465268 hasConceptScore W1998465268C2775924081 @default.
• W1998465268 hasConceptScore W1998465268C2778304055 @default.
• W1998465268 hasConceptScore W1998465268C29829512 @default.
• W1998465268 hasConceptScore W1998465268C33923547 @default.
• W1998465268 hasConceptScore W1998465268C34388435 @default.
• W1998465268 hasConceptScore W1998465268C38652104 @default.
• W1998465268 hasConceptScore W1998465268C41008148 @default.
• W1998465268 hasConceptScore W1998465268C47446073 @default.
• W1998465268 hasConceptScore W1998465268C5594486 @default.
• W1998465268 hasConceptScore W1998465268C62520636 @default.
• W1998465268 hasIssue "4" @default.
• W1998465268 hasLocation W19984652681 @default.
• W1998465268 hasOpenAccess W1998465268 @default.
• W1998465268 hasPrimaryLocation W19984652681 @default.
• W1998465268 hasRelatedWork W1541746961 @default.
• W1998465268 hasRelatedWork W1827747628 @default.
• W1998465268 hasRelatedWork W2094011599 @default.
• W1998465268 hasRelatedWork W2368484960 @default.

• next