Abstract
No AccessEngineering NoteHandling Qualities of a Twin Ducted-Fan Aircraft: An Analytical EvaluationOliver L. Grant, Karl A. Stol, Akshya Swain and Ronald A. HessOliver L. GrantDepartment of Mechanical Engineering, University of Auckland, Auckland 1010, New Zealand*Ph.D. Candidate, Department of Mechanical Engineering, Private Bag 92019.Search for more papers by this author, Karl A. StolDepartment of Mechanical Engineering, University of Auckland, Auckland 1010, New Zealand†Senior Lecturer, Department of Mechanical Engineering, Private Bag 92019. Senior Member AIAA.Search for more papers by this author, Akshya SwainDepartment of Mechanical Engineering, University of Auckland, Auckland 1010, New Zealand‡Senior Lecturer, Department of Electrical Engineering, Private Bag 92019.Search for more papers by this author and Ronald A. HessDepartment of Mechanical and Aeronautical Engineering, University of California, Davis, Davis, California 95616§Professor, Department of Mechanical and Aeronautical Engineering. Fellow AIAA.Search for more papers by this authorPublished Online:9 Jan 2015https://doi.org/10.2514/1.G000826SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations About References [1] Yoeli R., “The Operational Potential of Manned Ducted-Fan VTOL Vehicles,” International AeroTech Congress and Exhibition, SAE International, Grapevine, TX, 2005, pp. 1–6. doi:https://doi.org/10.4271/2005-01-3184 Google Scholar[2] Pflimlin J. M., Binetti P., Soueres P., Hamel T. and Trouchet D., “Modeling and Attitude Control Analysis of a Ducted-Fan Micro Aerial Vehicle,” Control Engineering Practice, Vol. 18, No. 3, March 2010, pp. 209–218. doi:https://doi.org/10.1016/2009.09.009 COEPEL 0967-0661 CrossrefGoogle Scholar[3] Flemming J. and Jones T., “Improving Control System Effectiveness for Ducted Fan VTOL UAVs Operating in Crosswinds,” 2nd AIAA “Unmanned Unlimited” Conference Workshop & Exhibit, AIAA Paper 2003-6514, 2003, pp. 1–6. doi:https://doi.org/10.2514/6.2003-6514 LinkGoogle Scholar[4] Mort K. W. and Yaggy P. F., “Aerodynamic Characteristics of a 4-Foot-Diameter Ducted Fan Mounted on the Tip of a Semispan Wing,” Technical Rept. NASA TND-1301, Huntsville, AL, 1962. Google Scholar[5] Weir R. J., “Aerodynamic Design Considerations for a Free-Flying Ducted Propeller,” AIAA Atmospheric Flight Mechanics Conference, AIAA Paper 88-4377-CP, 1988, pp. 420–431. doi:https://doi.org/10.2514/6.1988-4377 LinkGoogle Scholar[6] Akturk A., “Ducted Fan Inlet and Exit and Rotor Tip Flow Improvements for Vertical Lift Systems,” Ph.D. Dissertation, Aerospace Engineering Dept., Pennsylvania State Univ., University Park, PA, 2011. Google Scholar[7] Franz R., Milam M. and Hauser J., “Applied Receding Horizon Control of the Caltech Ducted Fan,” American Control Conference, Vol. 5, AACC, Anchorage, AK, 2002, pp. 3735–3740. doi:https://doi.org/10.1.1.63.7644 Google Scholar[8] Avanzini G., Ciniglio U. and Matteis G., “Full-Envelope Robust Control of a Shrouded-Fan Unmanned Vehicle,” Journal of Guidance, Control, and Dynamics, Vol. 29, No. 2, 2006, pp. 435–443. doi:https://doi.org/10.2514/1.14314 JGCDDT 0162-3192 LinkGoogle Scholar[9] Hess R. A. and Bakhtiari-Nejad M., “Sliding Mode Control of a Nonlinear Unmanned Aerial Vehicle Model,” Journal of Guidance, Control, and Dynamics, Vol. 31, No. 4, 2008, pp. 1163–1166. doi:https://doi.org/10.2514/1.32558 JGCDDT 0162-3192 LinkGoogle Scholar[10] Speck M., Buchholz J. and Sellier M., “A Mathematical Model of a Twin Ducted Fan VTOL Jetpack,” Proceedings of the Institution of Mechanical Engineers Part G: Journal of Aerospace Engineering, Vol. 228, No. 10, 2014, pp. 1831–1844. doi:https://doi.org/10.1177/0954410013503060 CrossrefGoogle Scholar[11] Speck M., “The Design, Theory, and Development of the Flight Envelope for a Twin-Ducted-Fan Jetpack,” Ph.D. Dissertation, Mechanical Engineering Dept., Canterbury Univ., Christchurch, New Zealand, 2013. Google Scholar[12] Anon., “ADS-33E-PRF, Aeronautical Design Standard, Performance Specification, Handling Qualities Requirements for Military Rotorcraft,” United States Army Aviation and Missile Command, Aviation Engineering Directorate, Redstone Arsenal, AL, March 2000. Google Scholar[13] Anon., “Aerospace-Flight Control Systems—Design, Instillation and Test of Piloted Military, General Specification,” SAE Aerospace Standard, July 2007. Google Scholar[14] Blanken C. L., Hoh R. H., Mitchell D. G. and Key D. L., “Test Guide for ADS-33E-PRF,” AMRDEC, Special Rept. AMR AF-08-07, July 2008. Google Scholar[15] Tischler M. B., Colbourne J. D., Morel M. R., Biezad D. J., Levine W. S. and Moldoveanu V., “CONDUIT—A New Multidisciplinary Integration Environment for Flight Control Development,” AIAA Guidance, Navigation and Control Conference, AIAA Paper 1997-3773, 1997, pp. 1756–1781. doi:https://doi.org/10.2514/6.1997-3773 LinkGoogle Scholar[16] Hess R. A., “Unified Theory for Aircraft Handling Qualities and Adverse Aircraft-Pilot Coupling,” Journal of Guidance, Control and Dynamics, Vol. 20, No. 6, 1997, pp. 1141–1148. doi:https://doi.org/10.2514/2.4169 LinkGoogle Scholar[17] Hess R. A. and Stout P. W., “Assessing Aircraft Susceptibility to Nonlinear Aircraft-Pilot Coupling/Pilot-Induced Oscillations,” Journal of Guidance, Control, and Dynamics, Vol. 21, No. 6, 1998, pp. 957–964. doi:https://doi.org/10.2514/2.4330 JGCDDT 0162-3192 LinkGoogle Scholar Previous article Next article
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