{"status":"ok","message-type":"work","message-version":"1.0.0","message":{"indexed":{"date-parts":[[2026,6,10]],"date-time":"2026-06-10T16:55:11Z","timestamp":1781110511735,"version":"3.54.1"},"reference-count":13,"publisher":"IGI Global Scientific Publishing","issue":"1","content-domain":{"domain":[],"crossmark-restriction":false},"short-container-title":[],"published-print":{"date-parts":[[2018,1]]},"abstract":"<jats:p>This article describes how one optimal design method is given to the design of missile autopilots. This method profits from an exhaustive method. By this method, the design process of a missile autopilot is simplified, and the design efficiency is improved. In the design process of this method, the performance indexes of autopilot are translated into constraint conditions, and the response speed is translated to an objective function. Thus, the optimal design of missile autopilot is translated into the optimal design of a nonlinear system with multiple constraints. The optimization algorithm is found to be out of controller parameter combinations which can satisfy constrained conditions. Firstly, calculations of the corresponding objective function values. Second, by the extract the optimal combination which has the minimal objective function value.<\/jats:p>","DOI":"10.4018\/ijeis.2018010106","type":"journal-article","created":{"date-parts":[[2018,1,29]],"date-time":"2018-01-29T12:21:42Z","timestamp":1517228502000},"page":"104-110","source":"Crossref","is-referenced-by-count":0,"title":["An Optimal Missile Autopilot Design Model"],"prefix":"10.4018","volume":"14","author":[{"given":"Yong-chao","family":"Chen","sequence":"first","affiliation":[{"name":"Electronic Engineering Department, Shijiazhuang Mechanical Engineering College, Shijiazhuang, China"}],"role":[{"vocabulary":"crossref","role":"author"}]},{"given":"Xin-bao","family":"Gao","sequence":"additional","affiliation":[{"name":"Electronic Engineering Department, Shijiazhuang Mechanical Engineering College, Shijiazhuang, China"}],"role":[{"vocabulary":"crossref","role":"author"}]},{"given":"Min","family":"Gao","sequence":"additional","affiliation":[{"name":"Electronic Engineering Department, Shijiazhuang Mechanical Engineering College, Shijiazhuang, China"}],"role":[{"vocabulary":"crossref","role":"author"}]},{"given":"Dan","family":"Fang","sequence":"additional","affiliation":[{"name":"Electronic Engineering Department, Shijiazhuang Mechanical Engineering College, Shijiazhuang, China"}],"role":[{"vocabulary":"crossref","role":"author"}]}],"member":"2432","reference":[{"key":"IJEIS.2018010106-0","doi-asserted-by":"crossref","unstructured":"Godbole, A. A. & Talole, S.E. (2011). Robust Feedback Linearization approach to pitch autopilot design. In Proceedings of the 2011 7th International Conference on MEMS, NANO and Smart Systems, November 4-6.","DOI":"10.4028\/www.scientific.net\/AMR.403-408.4667"},{"key":"IJEIS.2018010106-1","author":"X. Y.Meng","year":"2003","journal-title":"Elements of Missile Guided and Control System"},{"key":"IJEIS.2018010106-2","author":"Y.Ming","year":"2015","journal-title":"Guided and Control Technology of Field Rocket"},{"key":"IJEIS.2018010106-3","unstructured":"Robert, F. H., Francois-David, X. H., Richard, A., & Hever, M. (2013). Development and Flight Testing of a Model Based Autopilot Library for a Low Cost Unmanned Aerial System. In Proceedings of the AIAA Guidance, Navigation, and Control (GNC) Conference, August 19-22."},{"key":"IJEIS.2018010106-4","doi-asserted-by":"publisher","DOI":"10.1109\/IEEEGCC.2011.5752563"},{"issue":"7","key":"IJEIS.2018010106-5","first-page":"590","article-title":"Design the Description Function of Guidance System with Velocity Pursuit Guidance Law","volume":"27","author":"H.Shen","year":"2007","journal-title":"Transactions of Beijing Institute of Technology"},{"key":"IJEIS.2018010106-6","doi-asserted-by":"publisher","DOI":"10.2514\/1.50555"},{"key":"IJEIS.2018010106-7","unstructured":"Tomazic, T., & Matko, D. (2011). Model based UAV autopilot tuning. In Proceedings of the 8th WSEAS International Conference on Fluid Mechanics, January 29-31 (pp. 18-22)."},{"key":"IJEIS.2018010106-8","author":"J. L.Wang","year":"2007","journal-title":"Research on Airborne Guided Rockets Guidance and Control System Design"},{"issue":"2","key":"IJEIS.2018010106-9","first-page":"888","article-title":"Autopilot Fast Response Robustness Design with Damp Constraint","volume":"18","author":"J. L.Wang","year":"2006","journal-title":"Xitong Fangzhen Xuebao"},{"issue":"3","key":"IJEIS.2018010106-10","first-page":"239","article-title":"Analysis of a Three-Loop Autopilot","volume":"26","author":"J. L.Wang","year":"2006","journal-title":"Transactions of Beijing Institute of Technology"},{"issue":"10","key":"IJEIS.2018010106-11","first-page":"1723","article-title":"Control System Fast Response Robustness Design","volume":"29","author":"J. L.Wang","year":"2007","journal-title":"Journal of Systems Engineering and Electronics"},{"issue":"2","key":"IJEIS.2018010106-12","first-page":"32","article-title":"Control System Fast Response Design with Control Constraint. Journal of Projectiles, Rockets","volume":"27","author":"J. L.Wang","year":"2007","journal-title":"Missiles and Guidance"}],"container-title":["International Journal of Enterprise Information Systems"],"original-title":[],"language":"en","link":[{"URL":"https:\/\/www.igi-global.com\/viewtitle.aspx?TitleId=198432","content-type":"unspecified","content-version":"vor","intended-application":"similarity-checking"}],"deposited":{"date-parts":[[2022,5,5]],"date-time":"2022-05-05T15:51:27Z","timestamp":1651765887000},"score":1,"resource":{"primary":{"URL":"http:\/\/services.igi-global.com\/resolvedoi\/resolve.aspx?doi=10.4018\/IJEIS.2018010106"}},"subtitle":[""],"short-title":[],"issued":{"date-parts":[[2018,1]]},"references-count":13,"journal-issue":{"issue":"1"},"URL":"https:\/\/doi.org\/10.4018\/ijeis.2018010106","relation":{},"ISSN":["1548-1115","1548-1123"],"issn-type":[{"value":"1548-1115","type":"print"},{"value":"1548-1123","type":"electronic"}],"subject":[],"published":{"date-parts":[[2018,1]]}}}