Chongqing University of Technology
2023 Virtual Special Issue on Rocket and Missile
Simulation study on exhaust noise of a rocket engine with different thrust and jet types
Kinematic performance and influence on early warning system of hypersonic targets
Evaluation model of combat capability of formation ship to air missiles based on Lanchester equation
Effect of the aging of propellant charge on drop safety
Study on spatial position distribution of a dynamic detonation shock wave field
Aerodynamic numerical analysis of the three stage submunition separation scheme
Design and experimental analysis of the trajectory correction fuze isolation platform
Study on the initial external ballistics of airborne subsonic submunitions
Semi active dynamic vibration absorbers for rocket sleds based on magneto rheological dampers
Simplified algorithm of the missile launcher model with geometric features
Design of the missile attitude control system of the model under a high uncertainty
Design of the ballistic tracking system with real time correction of deflection speed
Simulation research on early warning of EODAS ballistic missiles
Design of rocket anti lightning reinforcement based on particle swarm optimization algorithm
Research on the influence of a curved tail on aerodynamic characteristics of a projectile
Numerical study on dynamic aerodynamic characteristics of rockets with different tail structures
Numerical simulation on energy output optimization of D shaped warhead charge
Research on the transfer alignment method of airborne miniature missiles
Adaptive integrated control for hypersonic variable inlet vehicle
Variant flight vehicle field of view constrained cooperative guidance law
Attitude control of morphing aircraft based on uncertain LPV system
Research on the pressure environment of missile head during concentric tube launch
Research on the damage to bridge structure and deck target by penetratingexplosive warhead
Design and experiment of aftereffect damage enhanced shaped charge warhead
Simulation of plasma sheath formation characteristics of hypersonic vehicle