Screen LibraryIntroduction to aircraft flight mechanics : performance, static stability, dynamic stability, classical feedback control, and state-space foundations /
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| Main Authors: | |
|---|---|
| Group Author: | ; ; ; |
| Published: |
American Institute of Aeronautics and Astronautics, Inc.,
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| Publisher Address: | Reston, Virginia : |
| Publication Dates: | [2014] |
| Literature type: | Book |
| Language: | English |
| Edition: | Second edition. |
| Series: |
AIAA education series
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| Subjects: | |
| Carrier Form: | xvii, 700 pages : illustrations (some color), forms ; 24 cm. |
| Bibliography: | Includes bibliographical references (page 681) and index. |
| ISBN: |
9781624102547 (hardback) : 1624102549 (hardback) |
| Index Number: | TL671 |
| CLC: | V32 |
| Call Number: | V32/Y42/2nd ed. |
| Contents: | 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 and control augmentation -- Bode, state space, and special topics -- A-10 insights -- Appendix A: Conversions -- Appendix B: Properties of the U.S. Standard Atmosphere -- Appendix C: Airfoil data -- Appendix D: T-38 performance data -- Appendix E: Selected Laplace transforms -- Appendix F: Cramer's Rule -- Appendix G: Developme |