{"status":"ok","message-type":"work","message-version":"1.0.0","message":{"indexed":{"date-parts":[[2026,7,24]],"date-time":"2026-07-24T17:12:31Z","timestamp":1784913151249,"version":"3.55.0"},"reference-count":28,"publisher":"Springer Science and Business Media LLC","issue":"2","license":[{"start":{"date-parts":[[2022,4,1]],"date-time":"2022-04-01T00:00:00Z","timestamp":1648771200000},"content-version":"tdm","delay-in-days":0,"URL":"https:\/\/www.springer.com\/tdm"},{"start":{"date-parts":[[2022,4,1]],"date-time":"2022-04-01T00:00:00Z","timestamp":1648771200000},"content-version":"vor","delay-in-days":0,"URL":"https:\/\/www.springer.com\/tdm"}],"content-domain":{"domain":["link.springer.com"],"crossmark-restriction":false},"short-container-title":["J Syst Sci Complex"],"published-print":{"date-parts":[[2022,4]]},"DOI":"10.1007\/s11424-022-1498-5","type":"journal-article","created":{"date-parts":[[2022,4,18]],"date-time":"2022-04-18T15:37:55Z","timestamp":1650296275000},"page":"604-622","update-policy":"https:\/\/doi.org\/10.1007\/springer_crossmark_policy","source":"Crossref","is-referenced-by-count":78,"title":["Fully Actuated System Approach for 6DOF Spacecraft Control Based on Extended State Observer"],"prefix":"10.1007","volume":"35","author":[{"given":"Qin","family":"Zhao","sequence":"first","affiliation":[],"role":[{"vocabulary":"crossref","role":"author"}]},{"given":"Guang-Ren","family":"Duan","sequence":"additional","affiliation":[],"role":[{"vocabulary":"crossref","role":"author"}]}],"member":"297","published-online":{"date-parts":[[2022,4,18]]},"reference":[{"issue":"9","key":"1498_CR1","doi-asserted-by":"publisher","first-page":"1192","DOI":"10.1049\/iet-cta.2011.0413","volume":"6","author":"F Zhang","year":"2012","unstructured":"Zhang F and Duan G R, Integrated translational and rotational finite-time maneuver of a rigid spacecraft with actuator misalignment, IET Control Theory & Applications, 2012, 6(9): 1192\u20131204.","journal-title":"IET Control Theory & Applications"},{"key":"1498_CR2","doi-asserted-by":"publisher","first-page":"154","DOI":"10.1016\/j.ast.2018.05.042","volume":"79","author":"Q Li","year":"2018","unstructured":"Li Q, Yuan J, Zhang B, et al., Disturbance observer based control for spacecraft proximity operations with path constraint, Aerospace Science and Technology, 2018, 79: 154\u2013163.","journal-title":"Aerospace Science and Technology"},{"issue":"6","key":"1498_CR3","doi-asserted-by":"crossref","first-page":"1462","DOI":"10.1109\/JAS.2019.1911621","volume":"6","author":"L Sun","year":"2019","unstructured":"Sun L, Saturated adaptive output-constrained control of cooperative spacecraft rendezvous and docking, IEEE\/CAA Journal of Automatica Sinica, 2019, 6(6): 1462\u20131470.","journal-title":"IEEE\/CAA Journal of Automatica Sinica"},{"key":"1498_CR4","doi-asserted-by":"publisher","first-page":"37","DOI":"10.1016\/j.isatra.2018.11.048","volume":"88","author":"Q Li","year":"2019","unstructured":"Li Q, Yuan J, and Zhang B, Extended state observer based output control for spacecraft rendezvous and docking with actuator saturation, ISA Transactions, 2019, 88: 37\u201349.","journal-title":"ISA Transactions"},{"issue":"9","key":"1498_CR5","first-page":"1885","volume":"46","author":"G R Duan","year":"2020","unstructured":"Duan G R, High-order system approaches: III. Observability and observer design, Acta Automatica Sinica, 2020, 46(9): 1885\u20131895.","journal-title":"Acta Automatica Sinica"},{"issue":"5","key":"1498_CR6","doi-asserted-by":"publisher","first-page":"952","DOI":"10.1080\/00207721.2020.1849863","volume":"52","author":"G R Duan","year":"2021","unstructured":"Duan G R, High-order fully actuated system approaches: Part III. Robust control and high-order backstepping, International Journal of Systems Science, 2021, 52(5): 952\u2013971.","journal-title":"International Journal of Systems Science"},{"issue":"5","key":"1498_CR7","doi-asserted-by":"publisher","first-page":"972","DOI":"10.1080\/00207721.2020.1849864","volume":"52","author":"G R Duan","year":"2021","unstructured":"Duan G R, High-order fully actuated system approaches: Part IV. Adaptive control and highorder backstepping, International Journal of Systems Science, 2021, 52(5): 972\u2013989.","journal-title":"International Journal of Systems Science"},{"issue":"10","key":"1498_CR8","doi-asserted-by":"publisher","first-page":"2129","DOI":"10.1080\/00207721.2021.1879964","volume":"52","author":"G R Duan","year":"2021","unstructured":"Duan G R, High-order fully actuated system approaches: Part V. Robust adaptive control, International Journal of Systems Science, 2021, 52(10): 2129\u20132143.","journal-title":"International Journal of Systems Science"},{"issue":"10","key":"1498_CR9","doi-asserted-by":"publisher","first-page":"2161","DOI":"10.1080\/00207721.2021.1879966","volume":"52","author":"G R Duan","year":"2021","unstructured":"Duan G R, High-order fully-actuated system approaches: Part VI. Disturbance attenuation and decoupling, International Journal of Systems Science, 2021, 52(10): 2161\u20132181.","journal-title":"International Journal of Systems Science"},{"issue":"1","key":"1498_CR10","doi-asserted-by":"publisher","first-page":"54","DOI":"10.1080\/00207721.2021.1937750","volume":"53","author":"G R Duan","year":"2022","unstructured":"Duan G R, High-order fully actuated system approaches: Part VIII. Optimal control with application in spacecraft attitude stabilisation, International Journal of Systems Science, 2022, 53(1): 54\u201373.","journal-title":"International Journal of Systems Science"},{"key":"1498_CR11","doi-asserted-by":"publisher","first-page":"11","DOI":"10.1016\/j.isatra.2016.02.022","volume":"63","author":"L Sun","year":"2016","unstructured":"Sun L, Huo W, and Jiao Z, Robust adaptive relative position and attitude control for spacecraft autonomous proximity, ISA Transactions, 2016, 63: 11\u201319.","journal-title":"ISA Transactions"},{"issue":"2","key":"1498_CR12","doi-asserted-by":"publisher","first-page":"684","DOI":"10.1109\/TCST.2017.2669145","volume":"26","author":"L Sun","year":"2018","unstructured":"Sun L and Zheng Z, Disturbance observer-based robust saturated control for spacecraft proximity maneuvers, IEEE Transactions on Control Systems Technology, 2018, 26(2): 684\u2013692.","journal-title":"IEEE Transactions on Control Systems Technology"},{"key":"1498_CR13","doi-asserted-by":"publisher","first-page":"585","DOI":"10.1016\/j.ast.2018.04.009","volume":"77","author":"M Mammarella","year":"2018","unstructured":"Mammarella M, Capello E, Park H, et al., Tube-based robust model predictive control for spacecraft proximity operations in the presence of persistent disturbance, Aerospace Science and Technology, 2018, 77: 585\u2013594.","journal-title":"Aerospace Science and Technology"},{"issue":"1","key":"1498_CR14","doi-asserted-by":"publisher","first-page":"2","DOI":"10.1109\/TAES.2017.2729978","volume":"54","author":"Q Hu","year":"2017","unstructured":"Hu Q, Shao X, and Chen W H, Robust fault-tolerant tracking control for spacecraft proximity operations using time-varying sliding mode, IEEE Transactions on Aerospace and Electronic Systems, 2017, 54(1): 2\u201317.","journal-title":"IEEE Transactions on Aerospace and Electronic Systems"},{"key":"1498_CR15","doi-asserted-by":"crossref","unstructured":"Huang Y and Jia Y, Nonlinear robust H\u221e tracking control for 6 DOF spacecraft formation with input saturation, Proceedings of 2016 IEEE 55th Conference on Decision and Control, Las Vegas, 2016.","DOI":"10.1109\/CDC.2016.7798339"},{"issue":"3","key":"1498_CR16","doi-asserted-by":"publisher","first-page":"900","DOI":"10.1109\/TIE.2008.2011621","volume":"56","author":"J Han","year":"2009","unstructured":"Han J, From PID to active disturbance rejection control, IEEE Transactions on Industrial Electronics, 2009, 56(3): 900\u2013906.","journal-title":"IEEE Transactions on Industrial Electronics"},{"key":"1498_CR17","doi-asserted-by":"publisher","first-page":"501","DOI":"10.1016\/j.actaastro.2018.01.021","volume":"145","author":"D Ran","year":"2018","unstructured":"Ran D, Chen X, Ruiter A D, et al., Adaptive extended-state observer-based fault tolerant attitude control for spacecraft with reaction wheels, Acta Astronautica, 2018, 145: 501\u2013514.","journal-title":"Acta Astronautica"},{"issue":"10","key":"1498_CR18","doi-asserted-by":"publisher","first-page":"4971","DOI":"10.1016\/j.jfranklin.2019.04.018","volume":"356","author":"L G Gong","year":"2019","unstructured":"Gong L G, Wang Q, and Dong C Y, Spacecraft output feedback attitude control based on extended state observer and adaptive dynamic programming, Journal of the Franklin Institute, 2019, 356(10): 4971\u20135000.","journal-title":"Journal of the Franklin Institute"},{"key":"1498_CR19","unstructured":"Gao Z, Scaling and bandwidth-parameterization based controller tuning, Proceedings of the American Control Conference, Denver, 2006."},{"issue":"2","key":"1498_CR20","doi-asserted-by":"publisher","first-page":"1425","DOI":"10.1109\/TIE.2016.2611573","volume":"64","author":"J Li","year":"2016","unstructured":"Li J, Xia Y, Qi X, et al., On the necessity, scheme, and basis of the linear-nonlinear switching in active disturbance rejection control, IEEE Transactions on Industrial Electronics, 2016, 64(2): 1425\u20131435.","journal-title":"IEEE Transactions on Industrial Electronics"},{"issue":"6","key":"1498_CR21","doi-asserted-by":"publisher","first-page":"420","DOI":"10.1016\/j.sysconle.2011.03.008","volume":"60","author":"B Z Guo","year":"2011","unstructured":"Guo B Z and Zhao Z, On the convergence of an extended state observer for nonlinear systems with uncertainty, Systems & Control Letters, 2011, 60(6): 420\u2013430.","journal-title":"Systems & Control Letters"},{"issue":"1","key":"1498_CR22","doi-asserted-by":"publisher","first-page":"3","DOI":"10.4173\/mic.2007.1.1","volume":"28","author":"R Kristiansen","year":"2007","unstructured":"Kristiansen R, Grtli E I, Nicklasson P J, et al., A model of relative translation and rotation in leader-follower spacecraft formations, Modeling, Identification and Control, 2007, 28(1): 3\u201313.","journal-title":"Modeling, Identification and Control"},{"issue":"7","key":"1498_CR23","first-page":"1333","volume":"46","author":"G R Duan","year":"2020","unstructured":"Duan G R, High-order system approaches: I. Fully-actuated systems and parametric designs, Acta Automatica Sinica, 2020, 46(7): 1333\u20131345.","journal-title":"Acta Automatica Sinica"},{"issue":"2","key":"1498_CR24","doi-asserted-by":"publisher","first-page":"422","DOI":"10.1080\/00207721.2020.1829167","volume":"52","author":"G R Duan","year":"2021","unstructured":"Duan G R, High-order fully actuated system approaches: Part I. Models and basic procedure, International Journal of Systems Science, 2021, 52(2): 422\u2013435.","journal-title":"International Journal of Systems Science"},{"issue":"14","key":"1498_CR25","doi-asserted-by":"publisher","first-page":"3091","DOI":"10.1080\/00207721.2021.1921307","volume":"52","author":"G R Duan","year":"2021","unstructured":"Duan G R, High-order fully actuated system approaches: part VII. Controllability, stabilisability and parametric designs, International Journal of Systems Science, 2021, 52(14): 3091\u20133114.","journal-title":"International Journal of Systems Science"},{"issue":"3","key":"1498_CR26","doi-asserted-by":"publisher","first-page":"574","DOI":"10.2514\/1.G004803","volume":"43","author":"Q Zhao","year":"2020","unstructured":"Zhao Q and Duan G, Finite-time concurrent learning adaptive control for spacecraft with inertia parameter identification, Journal of Guidance, Control, and Dynamics, 2020, 43(3): 574\u2013584.","journal-title":"Journal of Guidance, Control, and Dynamics"},{"issue":"6","key":"1498_CR27","doi-asserted-by":"publisher","first-page":"3691","DOI":"10.1109\/TAES.2021.3082705","volume":"57","author":"Q Zhao","year":"2021","unstructured":"Zhao Q and Duan G, Concurrent learning adaptive finite-time control for spacecraft with inertia parameter identification under external disturbance, IEEE Transactions on Aerospace and Electronic Systems, 2021, 57(6): 3691\u20133704.","journal-title":"IEEE Transactions on Aerospace and Electronic Systems"},{"key":"1498_CR28","volume-title":"Space Mission Analysis and Design","author":"J R Wertz","year":"1999","unstructured":"Wertz J R and Larson W J, Space Mission Analysis and Design, 3rd Edition, Microcosm Press, Torrance, CA, 1999.","edition":"3rd Edition"}],"container-title":["Journal of Systems Science and Complexity"],"original-title":[],"language":"en","link":[{"URL":"https:\/\/link.springer.com\/content\/pdf\/10.1007\/s11424-022-1498-5.pdf","content-type":"application\/pdf","content-version":"vor","intended-application":"text-mining"},{"URL":"https:\/\/link.springer.com\/article\/10.1007\/s11424-022-1498-5\/fulltext.html","content-type":"text\/html","content-version":"vor","intended-application":"text-mining"},{"URL":"https:\/\/link.springer.com\/content\/pdf\/10.1007\/s11424-022-1498-5.pdf","content-type":"application\/pdf","content-version":"vor","intended-application":"similarity-checking"}],"deposited":{"date-parts":[[2024,9,22]],"date-time":"2024-09-22T11:27:42Z","timestamp":1727004462000},"score":1,"resource":{"primary":{"URL":"https:\/\/link.springer.com\/10.1007\/s11424-022-1498-5"}},"subtitle":[],"short-title":[],"issued":{"date-parts":[[2022,4]]},"references-count":28,"journal-issue":{"issue":"2","published-print":{"date-parts":[[2022,4]]}},"alternative-id":["1498"],"URL":"https:\/\/doi.org\/10.1007\/s11424-022-1498-5","relation":{},"ISSN":["1009-6124","1559-7067"],"issn-type":[{"value":"1009-6124","type":"print"},{"value":"1559-7067","type":"electronic"}],"subject":[],"published":{"date-parts":[[2022,4]]},"assertion":[{"value":"16 December 2021","order":1,"name":"received","label":"Received","group":{"name":"ArticleHistory","label":"Article History"}},{"value":"11 January 2022","order":2,"name":"revised","label":"Revised","group":{"name":"ArticleHistory","label":"Article History"}},{"value":"18 April 2022","order":3,"name":"first_online","label":"First Online","group":{"name":"ArticleHistory","label":"Article History"}}]}}