论文信息 - Large Angle Maneuvering with an Asymmetric Aircraft: A Single Loop Control Formulation - 字舞流文

Large Angle Maneuvering with an Asymmetric Aircraft: A Single Loop Control Formulation

Manoranjan Sinha | Bijoy K. Mukherjee

[1] Yu Liu,et al. Multivariable Adaptive Control of NASA Generic Transport Aircraft Model with Damage , 2011 .

[2] Marios M. Polycarpou,et al. Backstepping-Based Flight Control with Adaptive Function Approximation , 2005 .

[3] Youdan Kim,et al. Nonlinear Adaptive Flight Control Using Backstepping and Neural Networks Controller , 2001 .

[4] Irene M. Gregory,et al. General Equations of Motion for a Damaged Asymmetric Aircraft , 2007 .

[5] Nandan Kumar Sinha,et al. Accessible Regions for Controlled Aircraft Maneuvering , 2013 .

[6] Manoranjan Sinha,et al. Modeling and Bifurcation Analysis of Combat Aircraft Dynamics under Lateral C.M. Shift , 2016 .

[7] Min-Jea Tahk,et al. Missile acceleration controller design using proportional–integral and non-linear dynamic control design method , 2012 .

[8] S. Sadati,et al. Backstepping Controller Design Using Neural Networks for a Fighter Aircraft , 2007, Eur. J. Control.

[9] Yu Liu,et al. Modeling and Model Reference Adaptive Control of Aircraft with Asymmetric Damage , 2009 .

[10] William L. Garrard,et al. Nonlinear inversion flight control for a supermaneuverable aircraft , 1992 .

[11] Sahjendra N. Singh. Asymptotically decoupled discontinuous control of systems and nonlinear aircraft maneuver , 1989 .