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Posts
- Category: Airplane Stability and Control, Second Edition (continued)
- Pusher Propeller Problems
- The Special Case of the Voyager
- Modern Canard Tactical Airplanes
- Evolution of the Equations of Motion
- Linearization
- Early Numerical Work
- Glauert’s and Later Nondimensional Forms
- Rotary Derivatives
- Stability Boundaries
- Wind, Body, Stability, and Principal Axes
- Laplace Transforms, Frequency Response, and Root Locus
- The Modes of Airplane Motion
- Literal Approximations to the Modes
- Time Vector Analysis
- Vector, Dyadic, Matrix, and Tensor Forms
- Atmospheric Models
- Integration Methods and Closed Forms
- Steady-State Solutions
- Equations of Motion Extension to Suborbital Flight
- Heading Angular Velocity Correction and Initialization
- Suborbital Flight Mechanics
- Additional Special Forms of the Equations of Motion
- The Elastic Airplane
- Aeroelasticity and Stability and Control
- The Semirigid Approach to Wing Torsional Divergence
- The Effect of Wing Sweep on Torsional Divergence
- Aileron-Reversal Theories
- Aileron-Reversal Flight Experiences
- Spoiler Ailerons Reduce Wing Twisting in Rolls
- Aeroelastic Effects on Static Longitudinal Stability
- Stabilizer Twist and Speed Stability
- Dihedral Effect of a Flexible Wing
- Finite-Element or Panel Methods in Quasi-Static Aeroelasticity
- Aeroelastically Corrected Stability Derivatives
- Mean and Structural Axes
- Normal Mode Analysis
- Quasi-Rigid Equations
- Control System Coupling with Elastic Modes
- Reduced-Order Elastic Airplane Models
- Second-Order Elastic Airplane Models
- Stability Augmentation
- Automatic Pilots in History
- The Systems Concept
- Frequency Methods of Analysis
- Early Experiments in Stability Augmentation
- The Northrop YB-49 Yaw Damper
- The Northrop F-89 Sideslip Stability Augmenter
- Transfer-Function Numerators
- Transfer-Function Dipoles
- Command Augmentation Systems
- 20.9.1 Roll-Ratcheting
- Superaugmentation, or Augmentation for Unstable Airplanes
- Propulsion-Controlled Aircraft
- The Advent of Digital Stability Augmentation
- Practical Problems with Digital Systems
- Time Domain and Linear Quadratic Optimization
- Linear Quadratic Gaussian Controllers
- Robust Controllers, Adaptive Systems
- Robust Controllers, Singular Value Analysis
- Decoupled Controls
- Flying Qualities Research Moves with the Times
- Empirical Approaches to Pilot-Induced Oscillations
- Compensatory Operation and Model Categories
- Crossover Model
- Pilot Equalization with the Crossover Model
- Algorithmic (Linear Optimal Control) Model
- The Crossover Model and Pilot-Induced Oscillations
- Gibson Approach
- Neal-Smith Approach
- Bandwidth-Phase Delay Criteria
- Landing Approach and Turn Studies
- Implications for Modern Transport Airplanes
- Challenge of Stealth Aerodynamics
- Faceted Airframe Issues
- Parallel-Line Planform Issues
- Shielded Vertical Tails and Leading-Edge Flaps
- Fighters Without Vertical Tails
- Very Large Aircraft
- The Effect of Folding Wings
- Altitude Response During Landing Approach
- Longitudinal Dynamics
- Roll Response of Large Airplanes
- Large Airplanes with Reduced-Static Longitudinal Stability
- Work Still to Be Done
- Short Biographies of Some Stability and Control Figures
- Category: All
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- Резак пропановый: ключевые особенности устройства
- Как в казино Вулкан играть с ПК и мобильных устройств
- Бонусы в онлайн-казино Вулкан Роял
- Обзор честного онлайн-казино
- Cветодиодная лента Arlight
- Обзорная экскурсия по Омску