Aircraft control and simulation
Stevens, Brian L.
Aircraft control and simulation Brian L. Stevens , Frank. L. Lewis - 2nd. ed. - Hoboken John Wiley - xvi, 664 p.
Resúmenes, al final de cada capítulo Apéndices e índice alfabético, al final del libro.
Introduction. Vector Kinematics. Matrix analysis of knematics. Geodesy, earth´s gravitation, terrestrial navigation. Rigid-Body dynamics. Summary The kinematics and dynamics of aircraft motion : Introduction. Basic aerodynamics. Aircraft forces and moments. Static analysis. The nonlinear aircraft model.Linear models and the stability derivatives. Summary. Modeling the aircraft : Introduction. State-space models. Transfer function models. Numerical solution of the state equations. Aircraft models for simulation. Steady-state flight. Numerical linearization. Aircraft dynamic behavior. Feedback control. Summary Modeling, design and simulation tools : Introduction. Aircraft rigid-body modes. The handiling-qualities requirements. Stability augmentation. COntrol augmentation systems. Autopilots. Nonlinear simulation. Summary. Aircraft dynamics and classical control design : Introduction. Assignment of closed-loop dynamics. Linear quadratic regulator with output feedback. Tracking a command. Modifying the performance index. Model-following desing. Linear quadratic design with full state feedback. Dynamic inversion desing. Summary. Modern design techniques : Introduction. Multivariable frequency-domian analysis. Robus output-feedback desgn. Observers and the kalman filter. LQG/Loop-transfer recovery. Summary. Robustness and multivariable frquencydomain techniques : Introduction. Simulation of digital controllers. Discretization of continuous controllers. Modified continuous design. Implementation considerations.. Summmry Digital control :
0471371459
Aircraft control and simulation Brian L. Stevens , Frank. L. Lewis - 2nd. ed. - Hoboken John Wiley - xvi, 664 p.
Resúmenes, al final de cada capítulo Apéndices e índice alfabético, al final del libro.
Introduction. Vector Kinematics. Matrix analysis of knematics. Geodesy, earth´s gravitation, terrestrial navigation. Rigid-Body dynamics. Summary The kinematics and dynamics of aircraft motion : Introduction. Basic aerodynamics. Aircraft forces and moments. Static analysis. The nonlinear aircraft model.Linear models and the stability derivatives. Summary. Modeling the aircraft : Introduction. State-space models. Transfer function models. Numerical solution of the state equations. Aircraft models for simulation. Steady-state flight. Numerical linearization. Aircraft dynamic behavior. Feedback control. Summary Modeling, design and simulation tools : Introduction. Aircraft rigid-body modes. The handiling-qualities requirements. Stability augmentation. COntrol augmentation systems. Autopilots. Nonlinear simulation. Summary. Aircraft dynamics and classical control design : Introduction. Assignment of closed-loop dynamics. Linear quadratic regulator with output feedback. Tracking a command. Modifying the performance index. Model-following desing. Linear quadratic design with full state feedback. Dynamic inversion desing. Summary. Modern design techniques : Introduction. Multivariable frequency-domian analysis. Robus output-feedback desgn. Observers and the kalman filter. LQG/Loop-transfer recovery. Summary. Robustness and multivariable frquencydomain techniques : Introduction. Simulation of digital controllers. Discretization of continuous controllers. Modified continuous design. Implementation considerations.. Summmry Digital control :
0471371459