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Flight Dynamics

Second Edition

Robert F. Stengel

PDF
ca. 159,99
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Princeton University Press img Link Publisher

Naturwissenschaften, Medizin, Informatik, Technik / Naturwissenschaften allgemein

Beschreibung

An updated and expanded new edition of an authoritative book on flight dynamics and control system design for all types of current and future fixed-wing aircraft

Since it was first published, Flight Dynamics has offered a new approach to the science and mathematics of aircraft flight, unifying principles of aeronautics with contemporary systems analysis. Now updated and expanded, this authoritative book by award-winning aeronautics engineer Robert Stengel presents traditional material in the context of modern computational tools and multivariable methods. Special attention is devoted to models and techniques for analysis, simulation, evaluation of flying qualities, and robust control system design.

Using common notation and not assuming a strong background in aeronautics, Flight Dynamics will engage a wide variety of readers, including aircraft designers, flight test engineers, researchers, instructors, and students. It introduces principles, derivations, and equations of flight dynamics as well as methods of flight control design with frequent reference to MATLAB functions and examples. Topics include aerodynamics, propulsion, structures, flying qualities, flight control, and the atmospheric and gravitational environment.

The second edition of Flight Dynamics features up-to-date examples; a new chapter on control law design for digital fly-by-wire systems; new material on propulsion, aerodynamics of control surfaces, and aeroelastic control; many more illustrations; and text boxes that introduce general mathematical concepts.

  • Features a fluid, progressive presentation that aids informal and self-directed study
  • Provides a clear, consistent notation that supports understanding, from elementary to complicated concepts
  • Offers a comprehensive blend of aerodynamics, dynamics, and control
  • Presents a unified introduction of control system design, from basics to complex methods
  • Includes links to online MATLAB software written by the author that supports the material covered in the book

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Schlagwörter

Algebraic Riccati equation, Katabatic wind, South Magnetic Pole, Pressure altitude, Aircraft, Phase margin, Edward Sabine, Pressure gradient, Pitching moment, Aileron, Root locus, Area rule, Ducted fan, Advance ratio, Adverse yaw, Describing function, Downwash, Wind tunnel, Vertical stabilizer, Static pressure, Wingtip device, Flight envelope, Kalman filter, Static margin, Aeroelasticity, Cartesian coordinate system, Torque, Adaptive control, Dihedral (aeronautics), Coefficient, Wing tip, Transfer function, Extended Kalman filter, Phugoid, Slip (aerodynamics), Yaw (rotation), Supercritical airfoil, Duffing equation, Pitch-up, Fuselage, Ground effect (aerodynamics), Stability derivatives, Dutch roll, Mach number, Steady flight, Amplitude, Supercruise, Aerodynamic center, Airfoil, Thrust reversal, Phase lag (rotorcraft), Dynamic pressure, Propulsive efficiency, Coanda effect, Transonic, Horizontal plane, Kulbit, Angle of attack, Lift coefficient, Wing twist, Aircraft flight control system, Supersonic speed, Limit cycle, Mach tuck, Reynolds number, Sound barrier, Stall (fluid mechanics), Flight level, Leading-edge extension, Polynomial chaos