FIELD: aiming equipment, applicable for realization of control of three-dimensional maneuver of flight vehicle in the process of which an aimed drop of load to the observed point of the ground surface is ensured. SUBSTANCE: additional production operations are instilled in the process of aiming, in particular, phase co-ordinates of movement of the flight vehicle on the predicted trajectory of its movement in a number of points are predicted, i. e. the problem of the load ballistics is solved repeatedly. The predicted wind drifts are calculated not only with due account made for the time of load drop, but also the time of predicted movement of the flight vehicle to each of the mentioned points of the predicted trajectory. The expressions for each of the points of the predicted drop of load and each curved line of "bursts" are represented in the form of a projection onto the horizontal plane of the cartographic coordinate system, the image of the calculated impact line is introduced of the field of vision of the pilot (navigator), controlling the flight vehicle the curve line of "bursts" on the observed point of the ground surface is superposed in advance, and at the moment of coincidence of the latter with the point of the beginning of the line of "bursts" the aimed drop of load is carried out. EFFECT: expanded range of conditions of use of flight vehicles at a drop of loads to the assigned and visually detected point of ground surface, enhanced speed of response and accuracy at release of loads from non-standard three-dimensional maneuver.
