Stochastic Approach to Robust Flight Control Design Using Hierarchy-Structured Dynamic Inversion
暂无分享,去创建一个
Junichiro Kawaguchi | Tetsujiro Ninomiya | Yoshikazu Miyazawa | J. Kawaguchi | Y. Miyazawa | Tetsujiro Ninomiya
[1] Robert F. Stengel,et al. Flight Control Design using Nonlinear Inverse Dynamics , 1986, 1986 American Control Conference.
[2] Yoshikazu Miyazawa. Design with multiple-delay-model and multiple-design-point approach , 1995 .
[3] George Meyer,et al. Application of nonlinear transformations to automatic flight control , 1984, Autom..
[4] Dan Bugajski,et al. Dynamic inversion: an evolving methodology for flight control design , 1994 .
[5] William L. Garrard,et al. Nonlinear inversion flight control for a supermaneuverable aircraft , 1992 .
[6] Robert F. Stengel,et al. Robust Nonlinear Control of a Hypersonic Aircraft , 1999 .
[7] Ernest J. Ohlmeyer,et al. Nonlinear missile autopilot design using time-scale separation , 1997 .
[8] Toshikazu Motoda,et al. Longitudinal Landing Control Law for an Autonomous Reentry Vehicle , 1999 .
[9] K. Glover,et al. Robustness Analysis of Nonlinear Flight Controllers , 2005 .
[10] Gary J. Balas,et al. Robust Dynamic Inversion for Control of Highly Maneuverable Aircraft , 1995 .
[11] R. Walker,et al. Nonlinear flight test trajectory controllers for aircraft , 1987 .
[12] Dale F. Enns,et al. Nonlinear control law with application to high angle-of-attack flight , 1992 .
[13] Kevin A. Wise,et al. Stability and flying qualities robustness of a dynamic inversion aircraft control law , 1996 .