A method for enhancing an aerodynamic performance of an unmanned projectile. The grooves are machined into the strike surface with tight tolerances. The feedback control includes at least a proportional control and a differential control.
Algorithmically generated prior art
A method for enhancing an aerodynamic performance of an unmanned projectile. The grooves are machined into the strike surface with tight tolerances. The feedback control includes at least a proportional control and a differential control.