Method for regulating trajectory of missiles involves on-site alteration of air-state, power lug is made for connection of drag coefficient from mach number in equation of motion for missile treated as punctiform mass

摘要

Method involves on-site alteration of air-state. Power lug is made for the connection of the drag coefficient from Mach number in the equation of motion for the missile treated as punctiform mass. The analytical solution of equation of motion leads either to numerically calculable double integral for flying time or to explicit formula for specific sizes with horizontal distance as unattached variable.