METHOD FOR FORMATION OF STABILIZATION AND HOMING SIGNAL OF MOVABLE CARRIER AND ON-BOARD HOMING SYSTEM FOR ITS REALIZATION

FIELD: homing systems of movable carriers. ^ SUBSTANCE: signals are formed that are proportional to the projections of the vector of the phantom linear acceleration and the projections of the vector of the absolute turning speed of the vector (line) of target sighting to the respective co-ordinate axes of the base antenna co-ordinate system. with the aid of the obtained signals with regard to the original information of assignment of the target or/and object of sighting and initial conditions of alignment of the inertial measurement of the parameters of the sighting vector determined are the signals proportional to the current values of the target sighting vector, i.e. the projections of the vector of the absolute linear speed of closure of the movable carrier with the target to the respective co-ordinate axes of the base antenna co-ordinate system, slant range of closure of the movable carrier to the target, components of the space angular target co-ordinate in the base antenna co-ordinate system, guide cosines of the mutual attitude of the base antenna co-ordinate system and the reference geocentric co-ordinate system linked by its, co-ordinate axis to the stationary target of/and to the sighting object located, for example, on the earth surface. At an absence of the location contact with the target or/and with the sighting object the obtained signals are converted to the stabilization signals of the movable carrier from its oscillations relative to its center of masses in the horizontal plane, in the vertical plane and in rolling, as well as to the homing signals of the movable carrier to the target proportional to the g-loads. At a search of the sighting object and at its tracking signals are formed in the main or built-in short-wave wave radiation chamber that are proportional to the components of the space angular co-ordinate of the sighting object and the slant range to the sighting object in the antenna co-ordinate system. An this case signals are determined that are proportional to the parameters of the trajectory fluctuations and the deforming actions of the movable carrier body an the spatial attitude of the antenna phase center relative to the target or/and the sighting object. With the use of these signals a signal is formed that is proportional to the phase of the reference function being the function of the module of the target sighting or/and object sighting vector in the shifted co-ordinate system, i.e. the slant range to the target or/and