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Stabilität
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Gramian Analysis of a Shrouded Rotor Micro Air Vehicle in Hover
Design of Flexible Propellers with Optimized Load-Distribution Characteristics
Simulation of Orbital Debris Impact on Porous Ceramic Tiles
Boundary-Layer Stability Analysis of the High Enthalpy Shock Tunnel Transition Experiments
Transition Onset Predictions for Oblique Breakdown in a Mach 3 Boundary Layer
Robust Higher-Order Sliding-Mode Finite-Time Control of Aeroelastic Systems
Effect of Ballonet Sloshing on the Stability Characteristics of an Airship
Geometric Control Approach to Longitudinal Stability of Flapping Flight
Stability Augmentation and Active Flutter Suppression of a Flexible Flying-Wing Drone
Multidisciplinary Approach to Assessing Actuation Power of a Hybrid Wing–Body
Spatial Stability Analysis of Subsonic Jets Modified for Low-Frequency Noise Reduction
Comment on “Partial Integrated Missile Guidance and Control with Finite Time Convergence”
Attitude Responses in Coupled Orbit-Attitude Dynamical Model in Earth–Moon Lyapunov Orbits
MATLAB-Based Flight-Dynamics and Flutter Modeling of a Flexible Flying-Wing Research Drone
Numerical Study of Microscale Monopropellant Fuel Injection Using Two-Phase Slug Formation
Nonlinear Aeroelastic Analysis with Inextensible Plate Theory Including Correlation with Experiment
Optimization of Aircraft Lifting Surfaces Using a Cellular Division Method
Shape-Stabilized Composite Phase-Change Materials Prepared with Stearic Acid and Active Carbon
Improved Linearized Breakup Model for the Liquid Sheets Produced by Swirl Atomizers
Spacecraft Swarm Finite-Thrust Cooperative Control for Common Orbit Convergence
Rugged, Scramjet Inlet Temperature and Velocity Sensor: Design and Ground Test
Large Strain Four-Point Bending of Thin Unidirectional Composites
Beam-Riding Flight of a Laser Propulsion Vehicle Using Actively Controlled Pulse
Handling Qualities Requirements for Future Personal Aerial Vehicles
Discrete-Roughness-Element-Enhanced Swept-Wing Natural Laminar Flow at High Reynolds Numbers
New Solutions for the Perturbed Lambert Problem Using Regularization and Picard Iteration
Transition Analysis for the Ascent Phase of HIFiRE-1 Flight Experiment
Unstructured Mesh Manipulation in Response to Surface Deformation
Modeling Human Pilot Adaptation to Flight Control Anomalies and Changing Task Demands
Forced and Aeroelastic Responses of Bird-Damaged Fan Blades: A Comparison and Its Implications
Traveling Crossflow Instability for the HIFiRE-5 Elliptic Cone
Control of Crossflow Transition at High Reynolds Numbers Using Discrete Roughness Elements
Experimental Validation of a Flight Simulation Model for Slightly Flexible Aircraft
New Method for Eigenvector-Sensitivity Analysis with Repeated Eigenvalues and Eigenvalue Derivatives
Smooth Sliding Mode Control for Missile Interception with Finite-Time Convergence
Aerodynamic Formulation for Stability Analysis of Lightly Cambered Airfoils in Cascade
Longitudinal Control Strategy for Hypersonic Accelerating Vehicles
Boundary-Layer Transition Experiment During Reentry of HIFiRE-1
Robust Flight Control Design for Linear Systems with Real Parameter Uncertainty
One-Equation Turbulence Model Based on Extended Bradshaw Assumption
Mapping the Influence of Acoustic Resonators on Rocket Engine Combustion Stability