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
The Design of Inertia Platform with Reverse Frame Normalizing Theory
The Decoupling Design of Aircraft Lateral Flight Control Systems with Eigenstructure Assignment