Stall/Spin Flight Test Techniques with COTS Model Aircraft and Flight Data Systems
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[1] S. M. Burk,et al. RADIO-CONTROLLED MODEL DESIGN AND TESTING TECHNIQUES FOR STALL/SPIN EVALUATION OF GENERAL-AVIATION AIRCRAFT , 1975 .
[2] P. W. Brown,et al. Investigations of Modifications to Improve the Spin Resistance of a High-Wing, Single-Engine, Light Airplane , 1989 .
[3] Ella M. Atkins,et al. Aerodynamic sensing for a fixed wing UAS operating at high angles of attack , 2012 .
[4] Or D. Dantsker,et al. Stall/Spin Mitigation Flight Testing with a Subscale Aerobatic Aircraft , 2013 .
[5] Ilan Kroo,et al. Approaches to Automatic Stall/Spin Detection Based on Small-Scale UAV Flight Testing , 2015 .
[6] D. J. Dicarlo,et al. Flight investigation of stall, spin and recovery characteristics of a low-wing, single-engine, T-tail light airplane , 1985 .
[7] W. T. Suit,et al. Spin tests of a single-engine, high-wing light airplane , 1982 .
[8] Or D. Dantsker,et al. Stall/spin flight testing with a subscale aerobatic aircraft , 2013 .
[9] Ralph D. Kimberlin,et al. Flight testing of fixed-wing aircraft , 2003 .
[10] J. R. Chambers,et al. Summary of NASA stall/spin research for general aviation configurations , 1986 .