{"status":"ok","message-type":"work","message-version":"1.0.0","message":{"indexed":{"date-parts":[[2025,4,24]],"date-time":"2025-04-24T05:27:06Z","timestamp":1745472426902,"version":"3.38.0"},"reference-count":26,"publisher":"SAGE Publications","issue":"6","license":[{"start":{"date-parts":[[2016,4,4]],"date-time":"2016-04-04T00:00:00Z","timestamp":1459728000000},"content-version":"tdm","delay-in-days":0,"URL":"https:\/\/journals.sagepub.com\/page\/policies\/text-and-data-mining-license"}],"content-domain":{"domain":["journals.sagepub.com"],"crossmark-restriction":true},"short-container-title":["Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering"],"published-print":{"date-parts":[[2016,7]]},"abstract":"<jats:p> Commonly, a non-cooperative space target is tracked using angle-only data. An approach utilised in many tracking problems is to perform an initial orbit determination (IOD) step and then transition to sequential estimation. In this paper, a space-based passive tracking strategy is proposed that combines IOD and sequential estimation. For the space-based IOD problem, a modified Laplace\u2019s method is derived, in which the non-spherical effect of Earth is considered and more than three pairs of angle measurements are fused. For the sequential estimation, a robust filtering algorithm, termed the robust square-root cubature Kalman filter, is developed. An adaptive factor is introduced in the developed algorithm, to ensure robustness to measurement malfunctions. Simulation results demonstrate that the proposed strategy can be used in actual engineering applications. <\/jats:p>","DOI":"10.1177\/0959651816637770","type":"journal-article","created":{"date-parts":[[2016,4,5]],"date-time":"2016-04-05T01:49:54Z","timestamp":1459820994000},"page":"551-561","update-policy":"https:\/\/doi.org\/10.1177\/sage-journals-update-policy","source":"Crossref","is-referenced-by-count":3,"title":["Space-based passive tracking of non-cooperative space target using robust filtering algorithm"],"prefix":"10.1177","volume":"230","author":[{"given":"Panlong","family":"Wu","sequence":"first","affiliation":[{"name":"School of Automation, Nanjing University of Science and Technology, China"}]},{"given":"Yang","family":"Zhou","sequence":"additional","affiliation":[{"name":"School of Automation, Nanjing University of Science and Technology, China"}]},{"given":"Xingxiu","family":"Li","sequence":"additional","affiliation":[{"name":"School of Science, Nanjing University of Science and Technology, China"}]}],"member":"179","published-online":{"date-parts":[[2016,4,4]]},"reference":[{"volume-title":"2007 AMOS technical conference","author":"Bloch JJ","key":"bibr1-0959651816637770"},{"volume-title":"Proceedings of the 19th AAS\/AIAA space flight mechanics meeting","author":"DeMars K","key":"bibr2-0959651816637770"},{"key":"bibr3-0959651816637770","doi-asserted-by":"publisher","DOI":"10.1007\/s10569-007-9065-x"},{"volume-title":"AIAA\/ICAS international air and space symposium and exposition","author":"Mark ED","key":"bibr4-0959651816637770"},{"key":"bibr5-0959651816637770","doi-asserted-by":"publisher","DOI":"10.1109\/7.640260"},{"key":"bibr6-0959651816637770","doi-asserted-by":"publisher","DOI":"10.1109\/7.543850"},{"key":"bibr7-0959651816637770","doi-asserted-by":"publisher","DOI":"10.1109\/70.210792"},{"issue":"2","key":"bibr8-0959651816637770","first-page":"309","volume":"13","author":"Sharma J","year":"2002","journal-title":"Lincoln Lab J"},{"key":"bibr9-0959651816637770","doi-asserted-by":"publisher","DOI":"10.1109\/TAES.2012.6237613"},{"key":"bibr10-0959651816637770","doi-asserted-by":"publisher","DOI":"10.1007\/s10569-004-6593-5"},{"volume-title":"Methods of orbit determination","year":"1965","author":"Escobal PR.","key":"bibr11-0959651816637770"},{"key":"bibr12-0959651816637770","unstructured":"Anderson JD. 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