Analysis and Development of a Total Energy Control System for a Large Transport Aircraft
Low Cost, Multifunctional Sensor for Vehicle's Inertial Navigation System
Low Cost, Multifunctional Sensor for Vehicle's Inertial Navigation System
Aeroelastic optimization of high aspect ratio wings using an exact dynamic stiffness matrix method
Aeroelastic Optimization of High Aspect Ratio Wings Using an Exact Dynamic Stiffness Matrix Method
Research and Development on the Parameterized Aeroengine Structural Scheme Design System
Optimum Flight Trajectory Guidance Based on Total Energy Control of Aircraft
The Design of Inertia Platform with Reverse Frame Normalizing Theory
The Decoupling Design of Aircraft Lateral Flight Control Systems with Eigenstructure Assignment
A New Data Extrapolation Algorithm with Application in Guidance and Target Recognition
Radar Target Modeling and Recognition Based on Scattering Centers
The Effectivity Analysis of Approximate Reasoning Models in Expert System
Optimum Design of High Aspect Ratio Wings Subject to Aeroelastic Constraints
A Study of Rockets as Passive Controllers
Gust Alleviation and Flutter Suppression of an Optimized Composite Wing with Active Control
Flutter Analysis of Composite Wings Using an Exact Dynamic Stiffness Matrix Method
Measuring Evidential Consistence by a Generalized Relative Entropy
Provincewide Monitoring of Truck Traffic using Automatic Vehicle Classifiers
Reference systems for laser beam quality and parameter measurements [2889-546]
Deep-etched multiphase level fractional Talbot grating [2885-560]
Prelase A-O mode-locked Cr:LiSAF laser pumped by flashlamp [2889-596]
Efficient method for resisting humidity into MBDCG holograms [2885-536]
Generation of 3D image from computer data with dot array rainbow hologram (Invited Paper) [2885-524]
High-Resolution Polarimetric Radar Targets Recognition Based on the Fractal Characterization
Approach to Reach High Range Resolution by Using Neural Networks
High Range Resolution MMW Radar Target Recognition Approaches with Application
Supermaneuverable flight control using dynamica-inversion-based neural networks
Nonlinear inversion dynamic neurocontrol method for flight decoupling control problems
Detection and isolation of control surface effectiveness failures
Electro-optic modulator with quasi-velocity matching [2997-27]
Thermal Stability Analysis of UV-Induced Fiber Bragg Gratings
Low Cost Cast Aluminum-Fly Ash Composites for Ultralight Automotive Application
Method for improving performance of IR focal plane array using microlens array [3099-12]
Numerical MHD Modeling of the Solar Driver for the Destabilization of a Coronal Helmet Streamer
Reliability predictions on fiber gratings through alternate methods