TY  - BOOK
AU  - Stevens, Brian L.
AU  - Lewis, Frank. L.
TI  - Aircraft control and simulation
SN  - 0471371459
CY  - Hoboken
PB  - John Wiley
N1  - Resúmenes, al final de cada capítulo; Apéndices e índice alfabético, al final del libro; The kinematics and dynamics of aircraft motion; Introduction. Vector Kinematics. Matrix analysis of knematics. Geodesy, earth´s gravitation, terrestrial navigation. Rigid-Body dynamics. Summary; Modeling the aircraft; Introduction. Basic aerodynamics. Aircraft forces and moments. Static analysis. The nonlinear aircraft model.Linear models and the stability derivatives. Summary; Modeling, design and simulation tools; 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; Aircraft dynamics and classical control design; Introduction. Aircraft rigid-body modes. The handiling-qualities requirements. Stability augmentation. COntrol augmentation systems. Autopilots. Nonlinear simulation. Summary; Modern design techniques; 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; Robustness and multivariable frquencydomain techniques; Introduction. Multivariable frequency-domian analysis. Robus output-feedback desgn. Observers and the kalman filter. LQG/Loop-transfer recovery. Summary; Digital control; Introduction. Simulation of digital controllers. Discretization of continuous controllers. Modified continuous design. Implementation considerations.. Summmry
ER  -