Introduction to aircraft flight mechanics : performance, static stability, dynamic stability, classical feedback control, and state-space foundations

Detalles Bibliográficos
Autor principal: Yechout, Thomas R.
Otros Autores: Morris, Steven L., 1952-, Bossert, David E., Hallgren, Wayne F., Hall, James K., 1969-
Formato: Libro
Lenguaje:English
Publicado: Reston, Virginia : American Institute of Aeronautics and Astronautics, Inc., ©2014.
Edición:Second edition.
Colección:AIAA education series.
Materias:
Aviones
Aerodinámica
Vuelo
Control de vuelo
Tabla de Contenidos:
  • 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: Development of longitudinal and lateral-directional transfer functions
  • Appendix H: Stability characteristics of selected aircraft.

Ejemplares similares