Introduction to Aircraft Flight Mechanics: Performance, Static Stability, Dynamic Stability, and Classical Feedback Control
@inproceedings{Yechout2003IntroductionTA, title={Introduction to Aircraft Flight Mechanics: Performance, Static Stability, Dynamic Stability, and Classical Feedback Control}, author={Thomas R. Yechout and Steven L. Morris}, year={2003} }
A Review of Basic Aerodynamics A Review of Basic Propulsion Aircraft Performance Aircraft Equations of Motion Aircraft Static Stability Linearizing the Equations of Motion Aircraft Dynamic Stability Classical Feedback Control Aircraft Stability/Control Augmentation Special Topics Appendices.
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References
SHOWING 1-10 OF 11 REFERENCES
Air Force Flight Evaluation (Systems) of the A-10A Prototype Aircraft
- Engineering
- 1973
Abstract : This report presents results of the systems evaluation portion of the A-10A prototype Air Force Flight Evaluation. The A-10A weapon system, as tested by the AFFTC, demonstrated or…
Design of Fuzzy Pitch Attitude Hold Systems for a Fighter Jet
- Engineering, Computer Science
- 2001
The design of fuzzy logic pitch attitude hold systems for an F-4 fighter jet under a variety of degraded performance conditions are described and a 25-rule fuzzy logic controller outperforms the conventional gain controller in terms of settling time, peak value, and steady state error for a step response in all cases.
Flight Stability and Automatic Control. R. C. Nelson. McGraw-Hill Book Company, New York. 1989. 284 pp. Illustrated. £27.95.
- ArtThe Aeronautical Journal (1968)
- 1989
Readers of prefaces in technical books will have seen many versions of: 'This book has grown out of lecture notes fo r . . .' and one need not check this preface to be convinced that the book has an…
Introduction to Aeronautics: A Design Perspective
- Engineering
- 1997
The most exciting moment for an aeronautical engineer is when his or her design becomes a working aircraft, the endpoint of a journey that begins in the classroom. Introduction to Aeronautics: A…
Low Speed Rotary Aerodynamic of F-18 Configuration for 0 to 90 Angle
- 1985
Attack—Test Results and Analysis,’
- NASA CR-3608,
- 1984
A-10A Prototype Task II Performance and Flying Qualities Evaluation,’
- Air Force Flight Test Center TR 73-7,
- 1973
Other 1940s era autopilots used on military aircraft
- 1940
Feedback and Control Systems, Schaum’s
- 1988