RU2822245C2 - Method for destroying underground targets with missiles separated from launch vehicle - Google Patents

Abstract

FIELD: missile guidance systems.

SUBSTANCE: In the defensive and offensive system (DOS), the coordinates and sizes of the areas of underground targets are taken from the outside, a launch vehicle (LV) is assigned to deliver missiles with ground-penetrating radars to the target areas and transmit the data of the LV, detachable missiles and ground-penetrating radars to the control station (CS), where the launch vehicle is launched. On the LV and missiles, their coordinates and velocities are determined and transmitted through the CS to the DOS, where the trajectories and speeds of the movement of the LV and missiles to the target areas are calculated and transmitted to the CS, where commands are formed to separate the missiles from the LV and transmit them to the LV, as well as form guidance commands for the LV and missiles and transmit them on the LV and missiles. On the CS, teams are formed to separate ground-penetrating radars from missiles and transfer them to missiles. On georadars, after landing, their coordinates are determined, as well as the coordinates and characteristic features of the targets, and they are transmitted through the CS to the DOS, where they determine the exact coordinates and characteristics of the targets, assign a LV with air-underground missiles to destroy targets and transmit the data of the PH and detachable missiles to the CS, where the LV is launched. On the LV and missiles, their coordinates and speeds in the air are determined and transmitted through the CS to the DOS, where the coordinates of the aiming points for missiles are determined, as well as the trajectories and speeds of the movement of the LV and missiles to targets are calculated and transmitted to the CS, where commands are formed to separate the missiles from the LV and transmit them to the LV. They form guidance commands for LV and missiles in the air and transmit them to the LV and missiles. The CS transmits calculated trajectories and speeds of missiles moving to targets underground to missiles, where after landing their coordinates and speeds are determined and missile guidance commands are formed underground, as well as detonating warheads at targets.

EFFECT: increase in the probability of destroying underground targets by missiles.

1 dwg

Description

The invention relates to missile guidance systems, namely defensive-offensive systems, and can be used to destroy group underground targets by groups of air-underground missiles separated from launch vehicles.

The closest to the proposed method is the method of destroying underground targets with missiles separated from the launch vehicle (RU 2775903), in which in the defensive-offensive system (ONS) the coordinates and dimensions of the areas where underground targets are located are received from the outside, and a launch vehicle (LV) is assigned for delivery missiles with ground penetrating radars to target areas and transmit data from launch vehicles, detachable missiles and ground penetrating radars to the control station (CS); LVs with missiles are launched at the control center; on the launch vehicle and detachable missiles, their current coordinates and velocities are determined and transmitted through the control system to the ONS; in the ONS they calculate the trajectories and speeds of movement of the launch vehicle and detachable missiles to the target areas and transmit them to the control system; commands are generated at the control system for separating missiles from the launch vehicle at the beginning of the calculated trajectories and transmit them to the launch vehicle; on the control system, commands are formed to guide the launch vehicle and separated missiles to the areas where the targets are located along the calculated trajectories with the calculated speeds and transmit them to the launch vehicle and missiles; at the control system, commands are formed for separating georadars from missiles separated from the launch vehicle at the end of the calculated trajectories and transmit them to the missiles; on georadars separated from the missiles, after landing, their coordinates are determined, as well as the coordinates and characteristic features of the targets, and transmit them through the control system to the ONS; the ONS determines the exact coordinates and characteristics of targets, assigns launch vehicles with missiles to destroy targets and transmits data from launch vehicles and detachable missiles to the control system; in the ONS, the coordinates of the aiming points for detachable missiles are determined; in the ONS they calculate the trajectories and speeds of movement of the launch vehicles and detachable missiles towards the targets and transmit them to the control system; commands are generated at the control system for separating missiles from the launch vehicle at the beginning of the calculated trajectories and transmit them to the launch vehicle; At the control system, commands are formed to guide the launch vehicle and separated missiles to targets along calculated trajectories with design speeds and transmit them to the launch vehicle and missiles.

However, this method does not provide the ability to select aiming points for missiles on the surface of targets, because they are underground, and this reduces the likelihood of targets being destroyed.

The purpose of the invention is to increase the likelihood of destroying underground targets by missiles.

The proposed method is that:

- the ONS receives from outside the coordinates and dimensions of the areas where underground targets are located, assigns the launch vehicle to deliver missiles with ground penetrating radars to the areas where the targets are located, and transmits data from the launch vehicle, detachable missiles and ground penetrating radars to the control system;

- launch vehicles with missiles are launched on the control system;

- on the launch vehicle and detachable missiles, their current coordinates and velocities are determined and transmitted through the control system to the ONS;

- the ONS calculates the trajectories and speeds of movement of the launch vehicles and detachable missiles to the target areas and transmits them to the control system;

- commands are generated at the control system for separating missiles from the launch vehicle at the beginning of the design trajectories and transmit them to the launch vehicle;

- on the control system, commands are formed to guide the launch vehicle and separated missiles to the areas where the targets are located along the calculated trajectories with the calculated speeds and transmit them to the launch vehicle and missiles;

- at the control system, commands are formed for separating georadars from missiles separated from the launch vehicle at the end of the calculated trajectories and transmit them to the missiles;

- on georadars separated from the missiles, after landing, their coordinates are determined, as well as the coordinates and characteristic features of the targets, and transmit them through the control system to the ONS;

- the ONS determines the exact coordinates and characteristics of targets, assigns launch vehicles with air-underground missiles to destroy targets and transmits data from launch vehicles and detachable missiles to the control system;

- launch vehicles with air-underground missiles are launched at the control center;

- on launch vehicles and detachable air-underground missiles, their current coordinates and velocities in the air are determined and transmitted through the control system to the ONS;

- in the ONS, the coordinates of the aiming points for detachable air-underground missiles are determined;

- the ONS calculates the trajectories and speeds of movement of launch vehicles and detachable air-underground missiles to targets and transmits them to the control system;

- commands are generated at the control system for separating air-underground missiles from the launch vehicle at the beginning of the calculated trajectories and transmit them to the launch vehicle;

- at the control system, commands are formed to guide the launch vehicle and separated air-underground missiles to targets along the air part of the calculated trajectories with design speeds and transmit them to the launch vehicle and missiles;

- the control system transmits the calculated trajectories and speeds of movement of separated air-underground missiles to targets underground to the missiles at the end of the air part of the calculated trajectories;

- on separated air-underground missiles, after landing, their current coordinates and speeds are determined and commands are generated to guide the missiles to targets along the underground part of the calculated trajectories with the calculated speeds;

- on separated air-underground missiles, warheads are detonated at the end of the underground part of the calculated trajectories.

ONS is similar to the well-known one (RU 2753498). The goals are similar to the known ones (RU 2761682). The coordinates and dimensions of target areas are taken from aerospace reconnaissance assets.

Launch vehicles, missiles and ground penetrating radars are prescribed based on their effectiveness. Georadars are similar to the well-known system (US 7948829) and consist of blocks spaced apart in space, with the help of each of which the coordinates and characteristic features of targets are determined. The exact coordinates and characteristics of targets are determined by analyzing their coordinates and characteristic features determined from various directions to the target using blocks in the georadars.

Air-underground missiles are similar to the well-known (ru.wikipedia.org, underground rocket). Aiming points for missiles are located on the surface of the targets. The coordinates of the aiming points are determined by selecting the most vulnerable spots of targets in accordance with their characteristics.

On launch vehicles and rockets, their coordinates and velocities are determined in on-board inertial navigation systems, corrected using a global satellite navigation system. On georadars, their coordinates are determined using a global satellite navigation system.

The trajectories and speeds of movement of launch vehicles and missiles are calculated from the condition of their bypass of third-party objects and enemy missile defense coverage areas, as well as from the condition of collision of ground penetrating radars with the ground and air-underground missiles with the ground and aiming points at the required angles with the required speeds. After the missiles are separated from the launch vehicle, targets are redistributed between them by adjusting the calculated trajectories and speeds.

The proposed method can be implemented in a system, the block diagram of which is shown in the drawing.

Blocks: 1 - ONS; 2 - SU; 3 - launch vehicle with missiles; 4 - missiles separated from the launch vehicle; 5 - georadars separated from missiles; 6 - launch vehicle with air-underground missiles; 7 - air-underground missiles, separated from the launch vehicle.

Connections between blocks: 1-2 - data on launch vehicles, detachable missiles and ground penetrating radars, calculated trajectories and speeds of movement of launch vehicles and detachable missiles to target areas, data from launch vehicles and detachable air-underground missiles, as well as calculated trajectories and speeds of movement of launch vehicles and detachable airborne missiles - underground missiles to targets; 2-1 - current coordinates and speed of the launch vehicle and detachable missiles, current coordinates and speeds of separated missiles, coordinates of separated georadars and coordinates and characteristic features of targets, current coordinates and speed of the launch vehicle and detachable air-underground missiles in the air, as well as current coordinates and speeds separated air-subterranean missiles in the air; 2-3 - commands for separating missiles from the launch vehicle at the beginning of the design trajectories, as well as commands for guiding the launch vehicle to the target areas along the design trajectory at the design speed; 2-4 - commands for guiding separated missiles to target areas along calculated trajectories with calculated speeds, as well as commands for separating georadars from missiles separated from the launch vehicle at the end of the calculated trajectories; 2-6 - commands for separating air-underground missiles from the launch vehicle at the beginning of the design trajectories, as well as commands for guiding the launch vehicle to targets along the design trajectory at the design speed; 2-7 - commands for guiding separated air-underground missiles to targets along the air part of the calculated trajectories with estimated speeds, as well as the calculated trajectories and speeds of movement of separated air-underground missiles to targets underground; 3-2 - current coordinates and speed of the launch vehicle and detachable missiles; 4-2 - current coordinates and velocities of separated missiles; 5-2 - coordinates of separated georadars and coordinates and characteristic features of targets; 6-2 - current coordinates and speed of the launch vehicle and detachable air-underground missiles in the air; 7-2 - current coordinates and velocities of separated air-underground missiles in the air; 8-1 - coordinates and sizes of areas where underground targets are located.

Claims (1)

A method of destroying underground targets with missiles separated from the launch vehicle, which consists in the fact that in a defensive-offensive system (ONS) the coordinates and dimensions of the areas where underground targets are located are received from the outside, a launch vehicle (LV) is assigned to deliver missiles with ground penetrating radars to the areas where they are located targets and transmit data from launch vehicles, detachable missiles and ground penetrating radars to the control station (CS); LVs with missiles are launched at the control center; on the launch vehicle and detachable missiles, their current coordinates and velocities are determined and transmitted through the control system to the ONS; in the ONS they calculate the trajectories and speeds of movement of the launch vehicle and detachable missiles to the target areas and transmit them to the control system; commands are generated at the control system for separating missiles from the launch vehicle at the beginning of the calculated trajectories and transmit them to the launch vehicle; on the control system, commands are formed to guide the launch vehicle and separated missiles to the areas where the targets are located along the calculated trajectories with the calculated speeds and transmit them to the launch vehicle and missiles; at the control system, commands are formed for separating georadars from missiles separated from the launch vehicle at the end of the calculated trajectories and transmit them to the missiles; on georadars separated from the missiles, after landing, their coordinates are determined, as well as the coordinates and characteristic features of the targets, and transmit them through the control system to the ONS; the ONS determines the exact coordinates and characteristics of targets, assigns launch vehicles with missiles to destroy targets and transmits data from launch vehicles and detachable missiles to the control system; in the ONS, the coordinates of the aiming points for detachable missiles are determined; in the ONS they calculate the trajectories and speeds of movement of the launch vehicles and detachable missiles towards the targets and transmit them to the control system; commands are generated at the control system for separating missiles from the launch vehicle at the beginning of the calculated trajectories and transmit them to the launch vehicle; at the control system, commands are formed to guide the launch vehicle and separated missiles to targets along calculated trajectories with design speeds and transmit them to the launch vehicle and missiles; characterized in that the ONS assigns air-underground missiles to destroy targets; LVs with air-to-underground missiles are launched at the SU; on launch vehicles and detachable air-underground missiles, their current coordinates and velocities in the air are determined and transmitted through the control system to the ONS; in the ONS, the coordinates of aiming points are determined for air-underground missiles; in the ONS, trajectories and speeds of movement towards targets are calculated for air-underground missiles; at the control system, teams of separation from the launch vehicle are formed for air-underground missiles; at the control system, target guidance commands are generated for air-underground missiles on the air part of the calculated trajectories; the control system transmits the calculated trajectories and speeds of movement of separated air-underground missiles to targets underground to the missiles at the end of the air part of the calculated trajectories; on separated air-underground missiles after landing, their current coordinates and speeds are determined and commands are generated to guide the missiles to targets along the underground part of the calculated trajectories with the calculated speeds; on separated air-underground missiles, warheads are detonated at the end of the underground part of the calculated trajectories.

Images