论文信息 - Analysis of Transition Stability for Morphing Aircraft - 字舞流文

Analysis of Transition Stability for Morphing Aircraft

T. M. Seigler | D. A. Neal

[1] Leonard Meirovitch,et al. Hybrid state equations of motion for flexible bodies in terms of quasi-coordinates , 1991 .

[2] P. Kokotovic,et al. On stability properties of nonlinear systems with slowly varying inputs , 1991 .

[3] D. Khusainov,et al. A method of determination of the solution of Lyapunov's equation with a prescribed spectrum , 1984 .

[4] T. Teichmann,et al. Dynamics of Flight: Stability and Control , 1959 .

[5] Brian Sanders,et al. Aerodynamic and Aeroelastic Characteristics of Wings with Conformal Control Surfaces for Morphing Aircraft , 2003 .

[6] C. Desoer,et al. Feedback Systems: Input-Output Properties , 1975 .

[7] J. N. Kudva,et al. Overview of the DARPA Smart Wing Project , 2004 .

[8] Wilson J. Rugh,et al. A stability result for linear parameter-varying systems , 1995 .

[9] Daniel J. Inman,et al. Modeling and Flight Control of Large-Scale Morphing Aircraft , 2007 .

[10] Wilson J. Rugh,et al. Analytical Framework for Gain Scheduling , 1990, 1990 American Control Conference.

[11] On Realization of Program Constraints: Part I—Theory , 1989 .