{"status":"ok","message-type":"work","message-version":"1.0.0","message":{"indexed":{"date-parts":[[2025,10,22]],"date-time":"2025-10-22T17:57:35Z","timestamp":1761155855104},"reference-count":27,"publisher":"Springer Science and Business Media LLC","issue":"1","license":[{"start":{"date-parts":[[2014,10,14]],"date-time":"2014-10-14T00:00:00Z","timestamp":1413244800000},"content-version":"tdm","delay-in-days":0,"URL":"http:\/\/www.springer.com\/tdm"}],"content-domain":{"domain":["link.springer.com"],"crossmark-restriction":false},"short-container-title":["J Intell Robot Syst"],"published-print":{"date-parts":[[2015,7]]},"DOI":"10.1007\/s10846-014-0126-6","type":"journal-article","created":{"date-parts":[[2014,10,13]],"date-time":"2014-10-13T00:59:41Z","timestamp":1413161981000},"page":"155-172","update-policy":"http:\/\/dx.doi.org\/10.1007\/springer_crossmark_policy","source":"Crossref","is-referenced-by-count":13,"title":["Modeling and Hovering Attitude Control of a Prototype Tandem Ducted Fan Vehicle"],"prefix":"10.1007","volume":"79","author":[{"given":"Yang","family":"Wang","sequence":"first","affiliation":[]},{"given":"Changle","family":"Xiang","sequence":"additional","affiliation":[]},{"given":"Yue","family":"Ma","sequence":"additional","affiliation":[]},{"given":"Xiaoliang","family":"Wang","sequence":"additional","affiliation":[]}],"member":"297","published-online":{"date-parts":[[2014,10,14]]},"reference":[{"key":"126_CR1","doi-asserted-by":"crossref","first-page":"629","DOI":"10.1007\/s10846-008-9279-5","volume":"54","author":"J Gadewadikar","year":"2009","unstructured":"Gadewadikar, J., Lewis, F.L., Subbarao, K., Peng, K., Chen, B.M.: H-Infinity Static Output-feedback Control for Rotorcraft. J. Intell. Robot. Syst. 54, 629\u2013646 (2009). doi: 10.1007\/s10846-008-9279-5","journal-title":"J. Intell. Robot. Syst."},{"key":"126_CR2","doi-asserted-by":"crossref","unstructured":"Marconi, L., Naldi, R.: Nonlinear robust control of a reduced-complexity ducted MAV for trajectory tracking. In: 44rd IEEE Conference on Decision Control, San Diego (2006)","DOI":"10.1109\/CDC.2006.377242"},{"key":"126_CR3","volume-title":"Ducted fan UAV modeling and simulation in preliminary design. In: AIAA modeling and simulation technologies conference and exhibit","author":"A Ko","year":"2007","unstructured":"Ko, A., Ohanian, O.J., Gelhausen, P.: Ducted fan UAV modeling and simulation in preliminary design. In: AIAA modeling and simulation technologies conference and exhibit. Hilton Head, South Carolina (2007)"},{"key":"126_CR4","doi-asserted-by":"crossref","unstructured":"Johnson, E.N., Turbe, M.A.: Modeling, control, and flight testing of a small ducted fan aircraft. In: Proceedings of the AIAA guidance, navigation and control conference and exhibit, San Francisco","DOI":"10.2514\/6.2005-6281"},{"key":"126_CR5","doi-asserted-by":"crossref","unstructured":"Marconi, L., Naldi, R., Gentili, L.: Modelling and control of a flying robot interacting with the environment 47, 2571\u20131583 (2011). doi: 10.1016\/j.automatica.2011.09.020","DOI":"10.1016\/j.automatica.2011.09.020"},{"key":"126_CR6","doi-asserted-by":"crossref","unstructured":"Colman, M.R., Suzuki, S., Kubo, D.: Wind Tunnel Test Results and Performance Prediction for a Ducted Fan with Collective and Cyclic Pitch Actuation for VTOL with Efficient Cruise.: In: AIAA Atmospheric Flight Mechanics Conference, Portland, Oregon (2011)","DOI":"10.2514\/6.2011-6379"},{"key":"126_CR7","doi-asserted-by":"crossref","unstructured":"Fleming, J., Jones, T., Ng, W.: Improving control system effectiveness for ducted fan VTOL UAVs operating in crosswinds. In: 2rd AIAA \u201dUnmanned Unlimited\u201d systems, Technologies, and Operations, San Diego, California","DOI":"10.2514\/6.2003-6514"},{"key":"126_CR8","doi-asserted-by":"crossref","first-page":"209","DOI":"10.1016\/j.conengprac.2009.09.009","volume":"18","author":"J-M Pflimlin","year":"2010","unstructured":"Pflimlin, J.-M., Binetti, P., Soueres, P.: Modeling and attitude control analysis of a ducted-fan micro aerial vehicle. Control. Eng. Pract. 18, 209\u2013218 (2010). doi: 10.1016\/j.conengprac.2009.09.009","journal-title":"Control. Eng. Pract."},{"key":"126_CR9","doi-asserted-by":"crossref","unstructured":"Ohanian, Osgar John, Gelhausen, Paul A.: A Compact Method for Modeling the Aerodynamics of Ducted Fan Vehicles. In: 48rd AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Orlando, Florida","DOI":"10.2514\/6.2010-1052"},{"issue":"5","key":"126_CR10","doi-asserted-by":"crossref","first-page":"666","DOI":"10.1080\/00207170601045034","volume":"80","author":"JM Pflimlin","year":"2005","unstructured":"Pflimlin, J.M., Soueres, P., Hamel, T.: Position control of a ducted fan VTOL UAV in crosswind. Int. J. Control. 80 (5), 666\u2013683 (2005). doi: 10.1080\/00207170601045034","journal-title":"Int. J. Control."},{"key":"126_CR11","doi-asserted-by":"crossref","unstructured":"McFarlane, D., Glover, K.: A loop shaping design procedure using H \u221e synthesis. IEEE Trans. Automat. Contr. 37(6), 759\u2013796 (1992)","DOI":"10.1109\/9.256330"},{"key":"126_CR12","doi-asserted-by":"crossref","DOI":"10.1007\/BFb0043199","volume-title":"Robust Controller Design Using Normalized Coprime Factor Plant Descriptions. Lecture Notes in Control and Information Sciences","author":"DC McFarlane","year":"1990","unstructured":"McFarlane, D.C., Glover, K.: Robust Controller Design Using Normalized Coprime Factor Plant Descriptions. Lecture Notes in Control and Information Sciences. Springer, Berlin (1990)"},{"key":"126_CR13","doi-asserted-by":"crossref","unstructured":"Tobias, E.L., Horn, J.F.: Simulation Analysis of the Controllability of a Tandem Ducted Fan Aircraft. In: AIAA Atmospheric Flight Mechanics Conference and Exhibit, Honolulu, Hawaii","DOI":"10.2514\/6.2008-6700"},{"key":"126_CR14","doi-asserted-by":"crossref","first-page":"48","DOI":"10.1016\/j.conengprac.2008.05.004","volume":"17","author":"K Iain","year":"2009","unstructured":"Iain, K., Peddle, T.J., Treurnicht, J.: Practical near hover flight control of a ducted fan (SLADe). Control. Eng. Pract. 17, 48\u201358 (2009). doi: 10.1016\/j.conengprac.2008.05.004","journal-title":"Control. Eng. Pract."},{"key":"126_CR15","doi-asserted-by":"crossref","unstructured":"Pflimlin, J.M., Soueres, P., Hamel, T.: Hovering flight stabilization in wind gusts for ducted fan UAV. In: 43rd IEEE Conference on Decision and Control, Atlantis, Paradise Island, Bahamas (2004)","DOI":"10.1109\/CDC.2004.1429251"},{"key":"126_CR16","doi-asserted-by":"crossref","first-page":"1971","DOI":"10.1016\/S0005-1098(01)00149-2","volume":"37","author":"J Yu","year":"2001","unstructured":"Yu, J., Jadbabaie, A., Primbs, J.: Comparison of nonlinear control design techniques on a model of the Caltech ducted fan. Automatica 37, 1971\u20131978 (2001)","journal-title":"Automatica"},{"issue":"2","key":"126_CR17","doi-asserted-by":"crossref","first-page":"435","DOI":"10.2514\/1.14314","volume":"29","author":"G Avanzini","year":"2006","unstructured":"Avanzini, G., Ciniglio, U., de Matteis, G.: Full-Envelope Robust Control of a Shrouded-Fan Unmanned Vehicle. AIAA J. Guid. Control Dyn. 29(2), 435\u2013443 (2006)","journal-title":"AIAA J. Guid. Control Dyn."},{"key":"126_CR18","unstructured":"John Koo, T., Sastry, S.: Output tracking control design of a helicopter model based on approximate linearization. In: 37rd Conference on Decision and Control, Florida (1998)"},{"key":"126_CR19","unstructured":"Gahinet, P., Nemirovski, A., Laub, A., Chilali, M.: LMI Control Tool Box. MATLAB., Mathworks, Inc., Natick, MA (1995)"},{"key":"126_CR20","unstructured":"Hyde, RA.: The application of robust control to VSTOL aircraft. Diss. University of Cambridge (1991)"},{"key":"126_CR21","doi-asserted-by":"crossref","unstructured":"Stiltner, B., John Ohanian, O.: Fan Angular Momentum Analysis for Ducted Fan UAVs During Conceptual Design.: In: 50rd AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Nashville, Tennessee (2012)","DOI":"10.2514\/6.2012-852"},{"key":"126_CR22","doi-asserted-by":"crossref","unstructured":"Prempain, E., Postlethwaite, I.: Static H loop shaping control of a fly-by-wire helicopter. In: 43rd IEEE Conference on Decision and Control, Atlantis, Paradise Island, Bahamas (2004)","DOI":"10.1109\/CDC.2004.1430203"},{"key":"126_CR23","doi-asserted-by":"crossref","first-page":"1517","DOI":"10.1016\/j.automatica.2005.04.001","volume":"41","author":"E Prempain","year":"2005","unstructured":"Prempain, E., Postlethwaite, I.: Static H loop shaping control of a fly-by-wire helicopter. Automatica 41, 1517\u20131528 (2005). doi: 10.1016\/j.automatica.2005.04.001","journal-title":"Automatica"},{"key":"126_CR24","unstructured":"Standard, A. D.: Performance Specification, Handling Qualities Requirements for Military Rotorcraft. US Army Aviation and Missile Command, Redstone Arsenal, AL, ADS-33E-PRF (2000)"},{"issue":"2","key":"126_CR25","doi-asserted-by":"crossref","first-page":"435","DOI":"10.2514\/1.14314","volume":"29","author":"G Avanzini","year":"2006","unstructured":"Avanzini, G., Ciniglio, U., de Matteis, G., Full-Envelope Robust Control of a Shrouded-Fan Unmanned Vehicle. J. Guid. Control. Dyn. 29(2), 435\u2013443 (2006). doi: 10.2514\/1.14314","journal-title":"J. Guid. Control. Dyn."},{"key":"126_CR26","volume-title":"Robust and optimal control","author":"K Zhou","year":"1996","unstructured":"Zhou, K., Doyle, J.C., Glover, K.: Robust and optimal control. Prentice Hall, New Jersey (1996)"},{"key":"126_CR27","volume-title":"Multivariable feedback control: analysis and design","author":"S Skogestad","year":"2007","unstructured":"Skogestad, S., Postlethwaite, I.: Multivariable feedback control: analysis and design. Wiley, New York (2007)"}],"container-title":["Journal of Intelligent &amp; Robotic Systems"],"original-title":[],"language":"en","link":[{"URL":"http:\/\/link.springer.com\/content\/pdf\/10.1007\/s10846-014-0126-6.pdf","content-type":"application\/pdf","content-version":"vor","intended-application":"text-mining"},{"URL":"http:\/\/link.springer.com\/article\/10.1007\/s10846-014-0126-6\/fulltext.html","content-type":"text\/html","content-version":"vor","intended-application":"text-mining"},{"URL":"http:\/\/link.springer.com\/content\/pdf\/10.1007\/s10846-014-0126-6","content-type":"unspecified","content-version":"vor","intended-application":"similarity-checking"}],"deposited":{"date-parts":[[2019,8,15]],"date-time":"2019-08-15T23:44:36Z","timestamp":1565912676000},"score":1,"resource":{"primary":{"URL":"http:\/\/link.springer.com\/10.1007\/s10846-014-0126-6"}},"subtitle":[],"short-title":[],"issued":{"date-parts":[[2014,10,14]]},"references-count":27,"journal-issue":{"issue":"1","published-print":{"date-parts":[[2015,7]]}},"alternative-id":["126"],"URL":"https:\/\/doi.org\/10.1007\/s10846-014-0126-6","relation":{},"ISSN":["0921-0296","1573-0409"],"issn-type":[{"value":"0921-0296","type":"print"},{"value":"1573-0409","type":"electronic"}],"subject":[],"published":{"date-parts":[[2014,10,14]]}}}