{"status":"ok","message-type":"work","message-version":"1.0.0","message":{"indexed":{"date-parts":[[2025,8,2]],"date-time":"2025-08-02T17:54:59Z","timestamp":1754157299880,"version":"3.41.2"},"reference-count":7,"publisher":"Emerald","issue":"1","license":[{"start":{"date-parts":[[2011,3,29]],"date-time":"2011-03-29T00:00:00Z","timestamp":1301356800000},"content-version":"tdm","delay-in-days":0,"URL":"https:\/\/www.emerald.com\/insight\/site-policies"}],"content-domain":{"domain":[],"crossmark-restriction":false},"short-container-title":[],"published-print":{"date-parts":[[2011,3,29]]},"abstract":"<jats:sec><jats:title content-type=\"abstract-heading\">Purpose<\/jats:title><jats:p>The purpose of this paper is to develop a novel type of full\u2010size flight control iron bird based on a passive electronic hydraulic servo loading system.<\/jats:p><\/jats:sec><jats:sec><jats:title content-type=\"abstract-heading\">Design\/methodology\/approach<\/jats:title><jats:p>On the basis of mathematical modeling of passive loading system math model, the detailed design process of the flight control iron bird is presented. Subsequently, the system digital simulation and physical verification are also given.<\/jats:p><\/jats:sec><jats:sec><jats:title content-type=\"abstract-heading\">Findings<\/jats:title><jats:p>Experimental results show that the proposed approach can reduce the redundant forces and improve the system dynamic and force\u2010tracking accuracy.<\/jats:p><\/jats:sec><jats:sec><jats:title content-type=\"abstract-heading\">Practical implications<\/jats:title><jats:p>This newly\u2010developed flight control iron bird system has been successfully applied in the flight control system design of some fighters.<\/jats:p><\/jats:sec><jats:sec><jats:title content-type=\"abstract-heading\">Originality\/value<\/jats:title><jats:p>The proposed approach for flight control iron bird is new and significant for the design of fighter flight control systems.<\/jats:p><\/jats:sec>","DOI":"10.1108\/17563781111115822","type":"journal-article","created":{"date-parts":[[2011,4,2]],"date-time":"2011-04-02T07:08:37Z","timestamp":1301728117000},"page":"111-137","source":"Crossref","is-referenced-by-count":4,"title":["Flight control iron bird based on passive electric\u2010hydraulic servo loading system"],"prefix":"10.1108","volume":"4","author":[{"given":"Yong","family":"Tian","sequence":"first","affiliation":[]},{"given":"Tian","family":"Li","sequence":"additional","affiliation":[]}],"member":"140","reference":[{"key":"key2022012420174953800_b1","doi-asserted-by":"crossref","unstructured":"Cieslak, J., Henry, D. and Zolghadri, A. (2010), \u201cFault tolerant flight control: from theory to piloted flight simulator experiments\u201d, IET Control Theory and Applications, Vol. 4, pp. 1451\u201061.","DOI":"10.1049\/iet-cta.2009.0146"},{"key":"key2022012420174953800_b2","doi-asserted-by":"crossref","unstructured":"Gerkens, T., Fritsch, G., Seyffert, C., B\u00fcttner, J., Mugtussidis, I. and Morrish, I. (2004), \u201cThe iron bird for the Fairchild\u2010Dornier 728\u201d, Aerospace Science and Technology, Vol. 8, pp. 231\u201043.","DOI":"10.1016\/j.ast.2003.11.004"},{"key":"key2022012420174953800_b3","doi-asserted-by":"crossref","unstructured":"Karpenko, M. and Sepehri, N. (2006), \u201cHardware\u2010in\u2010the\u2010loop simulator for research on fault tolerant control of electrohydraulic flight control systems\u201d, 2006 American Control Conference.","DOI":"10.1109\/ACC.2006.1657454"},{"key":"key2022012420174953800_b4","doi-asserted-by":"crossref","unstructured":"Parker, K. (1999), \u201cIs it a bird? Is it a plane? [pilot training simulator]\u201d, IEE Review, Vol. 45, pp. 178\u20109.","DOI":"10.1049\/ir:19990410"},{"key":"key2022012420174953800_b5","doi-asserted-by":"crossref","unstructured":"Patel, A.V., Patel, V.V. and Deodhare, G. et al. (2006), \u201cFlight control system clearance using static tests at iron bird\u201d, AIAA Guidance, Navigation, and Control Conference, Vol. 2, pp. 1308\u201018.","DOI":"10.2514\/6.2006-6203"},{"key":"key2022012420174953800_b6","doi-asserted-by":"crossref","unstructured":"Tan, C.F., Chen, W. and Boomen, V.D. et al. (2010), \u201cApplication of automation for low cost aircraft cabin simulator\u201d, 2010 International Conference on Control Automation and Systems (ICCAS), pp. 44\u20107.","DOI":"10.1109\/ICCAS.2010.5669948"},{"key":"key2022012420174953800_b7","unstructured":"Tian, Y. (2010), \u201cDesign and analysis of flight control iron\u2010bird test platform's electro\u2010hydraulic servo load system\u201d, PhD thesis, Beihang University, Beijing."}],"container-title":["International Journal of Intelligent Computing and Cybernetics"],"original-title":[],"language":"en","link":[{"URL":"http:\/\/www.emeraldinsight.com\/doi\/full-xml\/10.1108\/17563781111115822","content-type":"unspecified","content-version":"vor","intended-application":"text-mining"},{"URL":"https:\/\/www.emerald.com\/insight\/content\/doi\/10.1108\/17563781111115822\/full\/xml","content-type":"application\/xml","content-version":"vor","intended-application":"text-mining"},{"URL":"https:\/\/www.emerald.com\/insight\/content\/doi\/10.1108\/17563781111115822\/full\/html","content-type":"unspecified","content-version":"vor","intended-application":"similarity-checking"}],"deposited":{"date-parts":[[2025,7,24]],"date-time":"2025-07-24T23:44:23Z","timestamp":1753400663000},"score":1,"resource":{"primary":{"URL":"http:\/\/www.emerald.com\/ijicc\/article\/4\/1\/111-137\/133325"}},"subtitle":[],"short-title":[],"issued":{"date-parts":[[2011,3,29]]},"references-count":7,"journal-issue":{"issue":"1","published-print":{"date-parts":[[2011,3,29]]}},"alternative-id":["10.1108\/17563781111115822"],"URL":"https:\/\/doi.org\/10.1108\/17563781111115822","relation":{},"ISSN":["1756-378X"],"issn-type":[{"type":"print","value":"1756-378X"}],"subject":[],"published":{"date-parts":[[2011,3,29]]}}}