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Flugmechanik
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Nonlinear Stability Analysis Methods for Guided Artillery Projectiles (AIAA 2014-2541)
Rotorcraft Slope Landings with Articulated Landing Gear (AIAA 2013-5160)
Flight Stability and Control of Articulated Wing Aircraft (AIAA 2013-4982)
Design, Simulation, and Experimental Testing of Humanitarian Aid Airdrop Micro Packages
Parafoil Control Using Payload Weight Shift
Parametric Study of Powered Parafoil Flight Dynamics
Effects of Articulated Wings on the Stability of Small Unmanned Aircraft
Aerodynamic Effects of Parafoil Upper Surface Bleed Air Actuation
Smart Projectile State Estimation Using Evidence Theory
Projectile Monte-Carlo Trajectory Analysis Using a Graphics Processing Unit
Specialized System Identification for Autonomous Parafoil and Payload Systems
Estimation of Projectile Aerodynamic Coefficients Using Coupled CFD/RBD Simulation Results
Flight Stability of Asymmetric Projectiles with Control Mechanisms
Experimental Study of Gust Effects on Micro Air Vehicles
Flight Mechanics of a Novel Guided Spin-Stabilized Projectile Concept
Performance Characteristics of an Autonomous Airdrop System in Realistic Wind Environments
Use of Micro Spoilers for Control of Finned Projectiles
A variable stability projectile using an internal moving mass