Optimization design of the trajectory about gun-launched missile based on SQP

Engineering

• Impact Angle 100%
• Design Optimization 100%
• Simulation Result 33%
• Optimisation Problem 33%
• Flight Trajectory 33%
• Centerline 33%
• Homing Guidance 33%
• Terminal Guidance 33%
• Ignition Timing 33%
• Inclination Angle 33%