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Performance, stability, dynamics, and control of airplanes
Bandu N. Pamadi
- 14 Jan 2021
146
TL;DR: Performance, Stability, Dynamics and Control of Airplanes as mentioned in this paper provides a comprehensive and integrated overview of several interrelated disciplines involving airplane performance, including aerodynamics, dynamics, and control systems.
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Abstract: Performance, Stability, Dynamics and Control of Airplanes provides a comprehensive and integrated overview of several interrelated disciplines involving airplane performance It contains all necessary background material on aerodynamics, dynamics, and control systems, discussing the fundamental principles with the use of sketches, solved examples, and design exercises It is an ideal text for upper level undergraduates, graduate students, and professionals Chapters 1 through 3 present basic principles of aerodynamics, aircraft performance, and static equilibrium and control in steady flight Chapter 4 deals with aircraft dynamics and decoupled equations for longitudinal and lateral motion, and it introduces the concept of stability derivatives Chapter 5 discusses design of stability augmentation systems and autopilots Chapter 6 discusses aircraft response and methods of closed-loop control of aircraft, while Chapters 7 and 8 discuss problems of inertial coupling, aircraft spin, and high angle of attack The third edition features updates throughout along with a new chapter 9 on stability, control issues, and challenges of unmanned aerial vehicles
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Citations
Computational Methods for Aero-Structural Analysis and Optimisation of Aircrafts Based on Reduced-Order Structural Models
Lars Reimer,Georg Wellmer,Carsten Braun,Josef Ballmann +3 more
- 01 Jan 2009
TL;DR: In this paper, aeroelastic effects are introduced into the aerodynamic analysis of aircrafts by coupling DLR's flow solvers TAU and FLOWer to a Timoshenko-beam solver.
Robust stability analysis and topological dynamics of a nonminimum phase supersonic tactical missile
Belkacem Kada
- 25 May 2015
TL;DR: In this article, a non-minimum phase, model topologies, and poles mappings are derived via linearization of the SRTM dynamics, leading to internal instability and introducing a performance bound on the flight control system.
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Análisis computacional aerodinámico de Ala del Galápagos UAV
Alvarez Vinueza,D Alejandro +1 more
- 01 Jan 2014
TL;DR: In this article, the authors investigated the aerodynamic properties of the wing of a UAV and the effects of the downwash on the wing tip of the UAV with the use of the Reynolds Averaged Navier Stokes Equations.
•Dissertation
Contrôle d'un avion à stabilité réduite
Alexander Peter Feuersänger
- 01 Jan 2007
TL;DR: In this article, an ensemble of methodes and d'outils are evaluated to evaluate the impact of a reduction of the stabilite naturelle of an avion on its performance.
Computational dynamics of a light airplane
P. Chudý,Vladimir Danek +1 more
TL;DR: In this paper, the authors compared the results obtained from complex numerical simulation and analytical solutions of the aeroelastic response of an airplane to a beam-stick model and proven aerodynamic theory.
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