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Flugmechanik
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Aerodynamic Effects of Parafoil Upper Surface Bleed Air Actuation
AIAA-2003-5469 Stability and Control of a Projectile with an Internal Rotating Disk
A Nonlinear Model Predictive Observer for Smart Projectile Applications AIAA Paper
A Variable Stability Projectile Using an Internal Moving Mass
A variable stability projectile using an internal moving mass
Benefits of Autonomous Morphing Aircraft in Loiter and Attack Missions
Design, Simulation, and Experimental Testing of Humanitarian Aid Airdrop Micro Packages
Effects of Articulated Wings on the Stability of Small Unmanned Aircraft
Estimation of Projectile Aerodynamic Coefficients Using Coupled CFD/RBD Simulation Results
Experimental Study of Gust Effects on Micro Air Vehicles
Flight Dynamic Simulation for Multibody Aircraft Configurations
Flight Mechanics of a Novel Guided Spin-Stabilized Projectile Concept
Flight Stability and Control of Articulated Wing Aircraft (AIAA 2013-4982)
Flight Stability of Asymmetric Projectiles with Control Mechanisms
Improved Dispersion of a Fin Stabilized Projectile using a Passive Moveable Nose
Nonlinear Stability Analysis Methods for Guided Artillery Projectiles (AIAA 2014-2541)
Parafoil Control Using Payload Weight Shift
Parametric Study of Powered Parafoil Flight Dynamics
Performance Characteristics of an Autonomous Airdrop System in Realistic Wind Environments
Practical Assessment of Real-Time Impact Point Predictors for Smart Weapons
Projectile Monte-Carlo Trajectory Analysis Using a Graphics Processing Unit
Range Optimization of a Fin Stabilized Projectile
Rotorcraft Slope Landings with Articulated Landing Gear (AIAA 2013-5160)
Simulation of Two Projectiles Connected by a Flexible Tether
Smart Projectile State Estimation Using Evidence Theory
Specialized System Identification for Autonomous Parafoil and Payload Systems
The Effects of Liquid Payloads on the Trajectory of Spinning PRojectiles AIAA Paper
Time Dependent Effects of Liquid Moments on the Trajectory of Spinning Projectiles
Use of Micro Spoilers for Control of Finned Projectiles
Using CFD/RBD Results to Generate Aerodynamic Models for Projectile Flight Simulation AIAA Paper