Solving of the some special control problems of launch vehicle at the initial flight part using the AKOR method

Abstract

The paper is devoted to develop launch vehicle (LV) motion control algorithms for solution of the two special control problems at the initial flight part: controlled engines plumes displacement and LV emergency displacement in case of engine failure. The implementation of the displacement process in both tasks provides execution of specified preset programs. For formation controllers of the LV angular motion control system this paper proposes a modified version of analytical design of controllers (AKOR) problem solution. Efficiency of the developed control algorithms is verified by the simulation results of the algorithms as a part the detailed LV motion model.