{"status":"ok","message-type":"work","message-version":"1.0.0","message":{"indexed":{"date-parts":[[2025,3,2]],"date-time":"2025-03-02T05:35:25Z","timestamp":1740893725995,"version":"3.38.0"},"reference-count":21,"publisher":"SAGE Publications","issue":"2","license":[{"start":{"date-parts":[[2011,9,16]],"date-time":"2011-09-16T00:00:00Z","timestamp":1316131200000},"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":[[2012,2]]},"abstract":"<jats:p> In this paper, a general approach for robust partial stabilization of uncertain non-linear systems is presented. In this approach, the non-linear dynamic system is divided into two subsystems, called the first and the second subsystems. This division is done based on the required stability properties of the system\u2019s states. The reduced input vector (the vector that includes components of the input vector appearing in the first subsystem) is designed to asymptotically stabilize the first subsystem. The proposed scheme is then applied for designing a guidance law as a potential application. Indeed, the paper presents a new approach to the missile guidance problem and shows that asymptotic stability behaviour is not realistic for all states of the guidance system. The effectiveness of the proposed guidance law in interception of manoeuvring targets is demonstrated analytically and through computer simulations. <\/jats:p>","DOI":"10.1177\/0959651811413013","type":"journal-article","created":{"date-parts":[[2011,9,17]],"date-time":"2011-09-17T01:54:45Z","timestamp":1316224485000},"page":"233-242","update-policy":"https:\/\/doi.org\/10.1177\/sage-journals-update-policy","source":"Crossref","is-referenced-by-count":5,"title":["Robust partial control design for non-linear control systems: a guidance application"],"prefix":"10.1177","volume":"226","author":[{"given":"T","family":"Binazadeh","sequence":"first","affiliation":[{"name":"School of Electrical and Electronic Engineering, Shiraz University of Technology, Shiraz, Iran"},{"name":"Control and Intelligent Processing Center of Excellence, University of Tehran, Tehran, Iran"}]},{"given":"M-J","family":"Yazdanpanah","sequence":"additional","affiliation":[{"name":"School of Electrical and Electronic Engineering, Shiraz University of Technology, Shiraz, Iran"},{"name":"Control and Intelligent Processing Center of Excellence, University of Tehran, Tehran, Iran"}]}],"member":"179","published-online":{"date-parts":[[2011,9,16]]},"reference":[{"key":"bibr1-0959651811413013","doi-asserted-by":"publisher","DOI":"10.1016\/j.apm.2010.03.020"},{"key":"bibr2-0959651811413013","doi-asserted-by":"publisher","DOI":"10.1007\/s00034-009-9126-3"},{"issue":"1","key":"bibr3-0959651811413013","first-page":"10","volume":"35","author":"Rumyantsev V. 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