Dynamic Simulation Analysis of Shipborne Missile Launching under High-Wave-Level Environment
Study on Effect of Shipborne Missile Launch Position Based on Fast Fourier Transform
Analysis and Calculation of Tracked Vehicle Steering-Load Based on Conditions of Tracks' Slip
Research of CAN Bus Extension System Based on C8051F500 and SST39LF512
Study on the Impact of Missile Flight Mach to its Engine Thrust
Modal Analysis on the Simulation of the Missile Launchers Based on ABAQUS
Optimization Maneuver Strategy which Make the Loss of Height of UAV Minimum after Engine Stopped
Research on Initial Disturbance Influenced by Adapter Combined with Guide Rail
Design of the Tracked Vehicle Based on the STM32