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
An orthogonality sensitivity method for analytical dynamic model correction using modal test data
Optimum design of high aspect ratio wings subject to aeroelastic constraints
Optimum Design of High Aspect Ratio Wings Subject to Aeroelastic Constraints