Airplane Level Turn Performance, Including Stability Constraints, Using EBAC Method
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[1] P. R. Smith,et al. Using Bifurcation Methods to Aid Nonlinear Dynamic Inversion Control Law Design , 1998 .
[2] Lance W. Traub,et al. Effects of Spanwise Blowing on a Delta Wing with Vortex Flaps , 1995 .
[3] Yigang Fan,et al. Time-optimal lateral maneuvers of an aircraft , 1995 .
[4] E. Allgower,et al. Numerical Continuation Methods , 1990 .
[5] K. Sudhakar,et al. Prevention of jump in inertia-coupled roll maneuvers of aircraft , 1994 .
[6] Raman K. Mehra,et al. Bifurcation Analysis of Nonlinear Aircraft Dynamics , 1982 .
[7] N. Ananthkrishnan,et al. Inertia-coupled coordinated roll maneuvers of airplanes , 1995 .
[8] C. C. Jahnke,et al. Application of Bifurcation Theory to the High-Angle-of-Attack Dynamics of the F-14 , 1994 .
[9] John David Anderson,et al. Aircraft performance and design , 1998 .