Symmetric rocket guiding method, involves actuating actuating elements such that rocket accepts transverse accelerations, and periodically starting parameter detection, calculations and resulting controls of actuating elements

摘要

The method involves forming a hamiltonian function of an equation system, which is used to determine a movement of a focal point of a rocket (6). The hamiltonian function is solved in a pitch plane and a yaw plane of the rocket. Actuating elements (61) of the rocket are actuated in such a manner that the rocket accepts transverse accelerations calculated for points of time. Parameter detection, calculations and resulting controls of the actuating elements are periodically started. An independent claim is also included for a method for adjusting flight attitude of a symmetric rocket.