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