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Four degree of freedom missile motion equation based on proportional navigation method
- Four degree of freedom missile motion equation based on proportional navigation method,The motion equation of 4-DOF missile based on proportional guidance method is given, and the termination conditions are given
Missile Datcom 2011 GUI
- GUI version of missiledatcom. The aerodynamic parameters, including drag coefficient, lift coefficient and torque coefficient, can be calculated quickly by inputting missile shape parameters.