Aircraft Dynamics and Automatic Control
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★★★★★
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A01=Duane T. McRuer
A01=Dunstan Graham
A01=Irving Ashkenas
Actuator
Aerial refueling
Aerodynamic center
Aerodynamic force
Aerodynamics
Aeroelasticity
Aeronautics
Age Group_Uncategorized
Age Group_Uncategorized
Aileron
Air traffic control
Airborne early warning and control
Aircraft
Aircraft flight control system
Airfoil
Airframe
Airplane
Angle of attack
Aspect ratio (aeronautics)
Attitude control
Author_Duane T. McRuer
Author_Dunstan Graham
Author_Irving Ashkenas
Autocorrelation
automatic-update
Autopilot
Aviation
Category1=Non-Fiction
Category=TGMD4
Category=TRP
Category=TTDS
Center of gravity of an aircraft
Coefficient
COP=United States
Cruise (aeronautics)
Cruise control
Degrees of freedom (mechanics)
Delivery_Delivery within 10-20 working days
Dihedral (aeronautics)
Drag equation
eq_isMigrated=2
eq_non-fiction
eq_tech-engineering
Equations of motion
Fixed-wing aircraft
Flight control surfaces
Flight controller
Flight dynamics
Flight dynamics (fixed-wing aircraft)
Flight envelope
Flight instruments
Flight simulator
Flight test
Flying qualities
Helicopter
Helicopter flight controls
Helicopter rotor
Indicated airspeed
Inertial navigation system
Instrument landing system
Jet engine
Landing gear
Language_English
Loiter (aeronautics)
Mach number
Model aircraft
PA=Available
Phase lag (rotorcraft)
Phugoid
Piloting (navigation)
Price_€100 and above
PS=Active
Requirement
Right half-plane
Root locus
S-plane
Slip (aerodynamics)
softlaunch
Stability derivatives
Supersonic aircraft
Tail rotor
Takeoff
Takeoff and landing
Transfer function
Transponder (aeronautics)
Vehicle dynamics
Vertical plane
Vertical stabilizer
Washout (aeronautics)
Wing configuration
Product details
- ISBN 9780691600383
- Weight: 1106g
- Dimensions: 152 x 229mm
- Publication Date: 14 Jul 2014
- Publisher: Princeton University Press
- Publication City/Country: US
- Product Form: Paperback
- Language: English
Delivery/Collection within 10-20 working days
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Aeronautical engineers concerned with the analysis of aircraft dynamics and the synthesis of aircraft flight control systems will find an indispensable tool in this analytical treatment of the subject. Approaching these two fields with the conviction that an understanding of either one can illuminate the other, the authors have summarized selected, interconnected techniques that facilitate a high level of insight into the essence of complex systems problems. These techniques are suitable for establishing nominal system designs, for forecasting off-nominal problems, and for diagnosing the root causes of problems that almost inevitably occur in the design process. A complete and self-contained work, the text discusses the early history of aircraft dynamics and control, mathematical models of linear system elements, feedback system analysis, vehicle equations of motion, longitudinal and lateral dynamics, and elementary longitudinal and lateral feedback control. The discussion concludes with such topics as the system design process, inputs and system performance assessment, and multi-loop flight control systems. Originally published in 1974.
The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.
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