Vertical Aerospace Dynamics, Maciejowski example 5.8
The problem is to control the vertical-plane dynamics of an aircraft. There are 3 inputs, 3 outputs and five states.
- Maciejowski pp. 244-258, Plots on LQGLTR designs
- Maciejowski pp. Appendix pp 405-406, Describes the model.
- Hung and MacFarlane, Multivariable Feedback: A quasi-classical Approach, Lecture Notes in Control and Information Sciences, vol 40, Springer-Verlag