{"status":"ok","message-type":"work","message-version":"1.0.0","message":{"indexed":{"date-parts":[[2025,9,19]],"date-time":"2025-09-19T07:44:43Z","timestamp":1758267883083,"version":"3.41.2"},"reference-count":21,"publisher":"Wiley","issue":"1","license":[{"start":{"date-parts":[[2018,12,10]],"date-time":"2018-12-10T00:00:00Z","timestamp":1544400000000},"content-version":"vor","delay-in-days":343,"URL":"http:\/\/creativecommons.org\/licenses\/by\/4.0\/"}],"funder":[{"DOI":"10.13039\/501100001809","name":"National Natural Science Foundation of China","doi-asserted-by":"publisher","award":["61873319","61573161","61473124"],"award-info":[{"award-number":["61873319","61573161","61473124"]}],"id":[{"id":"10.13039\/501100001809","id-type":"DOI","asserted-by":"publisher"}]}],"content-domain":{"domain":["onlinelibrary.wiley.com"],"crossmark-restriction":true},"short-container-title":["Complexity"],"published-print":{"date-parts":[[2018,1]]},"abstract":"<jats:p>An integrated guidance integrated estimation\/guidance law is designed for exoatmospheric interceptors equipped with divert thrusters and optical seekers to intercept maneuvering targets. This paper considers an angles\u2010only guidance problem for exoatmospheric maneuvering targets. A bounded differential game\u2010based guidance law is derived against maneuvering targets using zero\u2010effort\u2010miss (ZEM). Estimators based the extended Kalman filter (EKF) and the unscented Kalman filter (UKF) are designed to estimate LOS rates that are contaminated by noise and target maneuver. Furthermore, to improve the observability of the range, an observability enhancement differential game guidance law is derived. The guidance law and the estimator are integrated together in the guidance loop. The proposed integrated estimation\/guidance law has been tested in several three\u2010dimensional nonlinear interception scenarios. Numerical simulations on a set of Monte\u2010Carlo simulations prove the validity and superiority of the proposed guidance law in hit\u2010to\u2010kill interception.<\/jats:p>","DOI":"10.1155\/2018\/7470823","type":"journal-article","created":{"date-parts":[[2018,12,10]],"date-time":"2018-12-10T23:32:03Z","timestamp":1544484723000},"update-policy":"https:\/\/doi.org\/10.1002\/crossmark_policy","source":"Crossref","is-referenced-by-count":2,"title":["Integrated Estimation\/Guidance Law against Exoatmospheric Maneuvering Targets"],"prefix":"10.1155","volume":"2018","author":[{"given":"Mao","family":"Su","sequence":"first","affiliation":[],"role":[{"role":"author","vocabulary":"crossref"}]},{"ORCID":"https:\/\/orcid.org\/0000-0003-3606-122X","authenticated-orcid":false,"given":"Lei","family":"Liu","sequence":"additional","affiliation":[],"role":[{"role":"author","vocabulary":"crossref"}]},{"ORCID":"https:\/\/orcid.org\/0000-0003-0161-1869","authenticated-orcid":false,"given":"Yongji","family":"Wang","sequence":"additional","affiliation":[],"role":[{"role":"author","vocabulary":"crossref"}]}],"member":"311","published-online":{"date-parts":[[2018,12,10]]},"reference":[{"key":"e_1_2_12_1_2","doi-asserted-by":"crossref","unstructured":"GutmanS.andRubinskyS. 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A ZEM Based Effective Integrated Estimation and Guidance of Interceptors Proceedings of the AIAA Guidance Navigation and Control and Co-located Conferences Portland Oregon American Institute of Aeronautics and Astronautics."},{"key":"e_1_2_12_19_2","doi-asserted-by":"crossref","unstructured":"DwivediP. TiwariS. BhattacharyaA. andPadhiR. A ZEM Dynamics Based Integrated Estimation Guidance and Control of Interceptors Proceedings of the AIAA Guidance Navigation and Control Conference Toronto Ontario Canada American Institute of Aeronautics and Astronautics https:\/\/doi.org\/10.2514\/6.2011-6420.","DOI":"10.2514\/6.2011-6420"},{"key":"e_1_2_12_20_2","doi-asserted-by":"publisher","DOI":"10.1177\/0954410014541079"},{"key":"e_1_2_12_21_2","unstructured":"Saroj KumarG. GhoseD. andVengadarajanA. 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