Control of ground objects escorting from aircraft

Abstract

The synthesis problem of adjuster for software automatic escorting of a ground mobile object using a surveysearch system of an aircraft is considered. The calculation of the control function is carried out by the method of the inverse dynamic problem separately for two angular channels. It is proposed to take into account the restrictions on the magnitude of the control action and on the angles of the line of sight, as well as to use the nonlinear Lewis equation with a correcting differential term as a reference equation. Keywords software support; synthesis of program control; method of the inverse dynamic problem