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Yaw Departure and Recovery of a Tailless Aircraft Configuration

2012; American Institute of Aeronautics and Astronautics; Volume: 50; Issue: 1 Linguagem: Inglês

10.2514/1.c031868

1533-3868

Gloria Stenfelt, Ulf Ringertz,

Dynamics and Control of Mechanical Systems

No AccessEngineering NoteYaw Departure and Recovery of a Tailless Aircraft ConfigurationGloria Stenfelt and Ulf RingertzGloria StenfeltDivision of Flight Dynamics, Royal Institute of Technology, SE-100 44 Stockholm, Sweden and Ulf RingertzDivision of Flight Dynamics, Royal Institute of Technology, SE-100 44 Stockholm, SwedenPublished Online:29 Jan 2013https://doi.org/10.2514/1.C031868SectionsView Full TextPDFPDF Plus ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Foster J. V., Cunningham K., Fremaux C. M., Shah G. H., Stewart E. C., Rivers R. A., Wilborn J. E. and Gato W., "Dynamics Modeling and Simulation of Large Transport Airplanes in Upset Conditions," AIAA Paper 2005-5933, Aug. 2005. LinkGoogle Scholar[2] Cummings R. M. and Schütte A., "An Integrated Computational/Experimental Approach to UCAV Stability & Control Estimation: Overview of NATO RTO AVT-161," AIAA Paper 2010-4392, July 2010. Google Scholar[3] Brinker J. S. and Wise K. A., "Flight Testing of Reconfigurable Control Law on the X-36 Tailless Aircraft," Journal of Guidance, Control, and Dynamics, Vol. 24, No. 5, 2001, pp. 903–909. doi:https://doi.org/10.2514/2.4826 JGCDDT 0162-3192 LinkGoogle Scholar[4] Stenfelt G. and Ringertz U., "Lateral Stability and Control of a Tailless Aircraft Configuration," Journal of Aircraft, Vol. 46, No. 6, 2009, pp. 2161–2163. doi:https://doi.org/10.2514/1.41092 JAIRAM 0021-8669 LinkGoogle Scholar[5] Stenfelt G. and Ringertz U., "Yaw Control of a Tailless Aircraft Configuration," Journal of Aircraft, Vol. 47, No. 5, 2010, pp. 1807–1810. doi:https://doi.org/10.2514/1.C031017 JAIRAM 0021-8669 LinkGoogle Scholar[6] Sträng G., "Fpl 35 Superstall och Spinn," Flight Mechanics Dept. TR L-35-1 B161, Saab AB, Linköping, Sweden, 1977. Google Scholar[7] Montgomery R. and Moul M., "Analysis of Deep-Stall Characteristics of T-Tailed Aircraft Configurations and Some Recovery Procedures," Journal of Aircraft, Vol. 3, No. 6, 1966, pp. 562–566. doi:https://doi.org/10.2514/3.43777 JAIRAM 0021-8669 LinkGoogle Scholar[8] Etkin B. and Reid L. D., Dynamics of Flight, Stability and Control, Wiley, New York, 1996. Google Scholar Previous article Next article