METHOD FOR PROVISION OF START OF ROCKET AT INITIAL SECTION OF TRAGECTORY FROM START CONSTRUCTION WITH OVERALL DIMENSION POINTS

摘要

A method for provision of start of rocket at initial section of trajectory from start construction with overall dimension points is based on determination of parameters of linear displacement of center of mass and angular deflection of rocket and use of executive devices of control system of rocket for reaction of deflections. After rocket goes out of boundaries of overall dimension points of launch construction one restricts actions of executive devices used for zeroing angular deflections of rocket in channels of pitch and jaw, by value 10 % for heave class rockets and up to 80 % for light class rockets from maximal possible.