Lateral Dynamics of Aeroplane
The problem is to design a state feedback controller u = -Lx.
There are two input signals (rudder and aileron) and 6 states.
- Anderson, Moore, Optimal Control, Linear quadratic methods,
2nd ed, Prentice Hall 1990, Sec 6.2
- Harvey and Stein, Quadratic Weights for Regulator Properties, IEEE AC 1978, pp 378-387
- Friedland, Control System Design, pp. 40-47. Nice description of Aerodynamics for control