A novel attitude control technique for miniature spacecraft
Synthese und Analyse im parametrischen Flugzeugvorentwurf
Design loads for future aircraft : = Les charges de calcul pour de futurs aéronefs
System identification modeling of a small-scale unmanned rotorcraft for flight control design
Flight test identification of SH-2G flapped-rotor helicopter flight mechanics models
Survey of TIGER main rotor loads from design to flight test
The Wright Brothers: First aeronautical engineers and test pilots
Dynamic analysis of flexible supercavitating vehicles using modal based elements
Complex configuration meshing - an industrial view and approach
Optimization of asymmetric oblique flying wing configurations under variable constraints
Incorporation of aircraft performance considerations in inverse airfoil design
Higher order staggered coupling schemes to predict the aeroelastic behavior of helicopter rotors