This thorough discussion of the classical stability and control theory of aircraft helps readers gain an appreciation of flight control systems. They will learn how to analyze and evaluate aircraft flying qualities and initiate preliminary augmentation design, as well as develop a foundation from which to move onto non-linear flight dynamics, simulation, and flight control.
- ISBN10 047023590X
- ISBN13 9780470235904
- Publish Date 16 March 1998
- Publish Status Out of Print
- Out of Print 15 December 2011
- Publish Country US
- Imprint John Wiley & Sons Inc
- Format Paperback
- Pages 380
- Language English