Aerodynamic Reduced-Order Models Based on Observer Techniques
Aeroelastic Wind Tunnel Test for Aerodynamic Uncertainty Model Validation
AEROSERVOELASTIC OPTIMIZATION OF A HIGH ASPECT TRANSPORT WING WITH MORPHING TRAILING EDGE
AIAA-2002-5753 The GPS Receiver for Micro/Nanosatellites
A Robust Roll Damping Controller
Comparison of Different RRD Controller Structures
Design and Analysis of a Wind Tunnel Test Model System for Gust Alleviation of Aeroelastic Aircraft
Development Trend Analysis of Automobile Electronic System F2012-D02-024
Divergence Experiment Prediction Techniques of Flat-Plate Forward-Swept Wing in Wind Tunnel
Dynamic Response Analysis and Experimental Validation for Airdrop of a Flexible Aircraft
Identification for Uncertain Aeroelastic System Set in the Frequency Domain