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Flugmechanik
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Basic Flight Mechanics : a simple Approach without Equations
Physik des Fliegens, Strömungsphysik, Raketen, Satelliten
Flugstabilität und Steuerbarkeit von Otto Lilienthals Normalsegelapparat von 1893
Advanced UAV aerodynamics, flight stability and control : novel concepts, theory and applications
Simulation of Flight Dynamics with an Improved Post-Stall Aerodynamics Model
Design, Simulation, and Experimental Testing of Humanitarian Aid Airdrop Micro Packages
Eigenvalue Constraints for Realization-Based Identification
Investigation of Trajectory Generation for a Mission Adaptive Planetary Entry Guidance Algorithm
Safe Set Maneuverability of Impaired Aircraft
LQR Controller for Stabilization of Flapping Wing MAV in Gust Environments
Ground Vibration Test Identified Structure Model for Flutter Envelope Prediction
Parafoil Control Using Payload Weight Shift
Robust Parafoil Terminal Guidance Using Massively Parallel Processing
Parametric Study of Powered Parafoil Flight Dynamics
Nonlinear Unsteady Aerodynamic Modeling by Volterra Variational Approach
Parameter Estimation of Highly Unstable Aircraft Assuming Linear Errors
Parametric Modeling for Store Separation Aerodynamics Using System Identification
Introduction to tensor flight dynamics : a paradigm shift
Flight theory and aerodynamics : a practical guide for operational safety
Helicopter aerodynamics / Ray Prouty ; Volume 3: Ray Prouty's Vertiflite Magazine columns 1990-2013
Solution methods for variational problems of low thrust space flight mechanics
Towards Industrialisation of Bifurcation Analysis in Rotorcraft Aeroelastic Problems
Design and Experimental Validation of a Control System for a Morphing Wing
The Bifurcation and Continuation Method from an Aerospace Systems Design Point of View
Aircraft Stall Phenomenon Analysis Using Nonlinearity Index Theory
Effect Of Jump Strut Nose Landing Gear In Preliminary Design Of Aircraft
Bifurcation Analysis of a Coupled Nose Landing Gear-Fuselage System
A Conceptual Study of Airfoil Performance Enhancement Using CFD
Bifurcation Analysis of the Generic Transport Model with a View to Upset Recovery
Method for Analyzing The Influence of Random Factors in Carrier Launching
Real-Time Frequency Response Estimation Using Multi-Sine Inputs and Recursive Fourier Transform