STUDY ON BALLISTIC OPTIMIZATION FOR EXTENDED RANGE GUIDED PROJECTILE

摘要

Long-range guided Projectile are characteristic of large flying area, further round andordinate high point. In favor of the cope of high-low height aerodynamic parameter, eachinter-channel remain nonlinear coupling in the course of movement. The design method ofclassical control theory is no longer true of long-range guidance shell control system. Forthe purpose of exert long-range guidance shell optimum performance, the text is base ofexterior ballistics theory, on basis of the analysis trajectory characteristic of long-rangeguidance projectile, adopt advanced design means of control system, to design andemulation count the ballistic optimize problem parting from the without control segmentand control segment two versus, the versus is proven that it has come to the best efficiencyto control shell flying position to long distance precision attack.