Method of target register using quadcopter
FIELD: weapons and ammunition.
SUBSTANCE: target register (1) is performed using a quadcopter (3) with a video camera (2) and a control panel with a tablet (4). The scale of the video image is determined in the region of the target by measurements of the distance in millimetres between the points of break of two near-point smoke ammunitions on the tablet, shooting of ammunitions is carried out with the installations of the sights which differ by 200 m. Longitudinal deviations and direction of impact point of the second register ammunition is measured on the tablet in mm with regard to the target and with the consideration of scale. The calculated corrections with the consideration of deviations received on the video image are introduced in sight for a shot with a live ammunition.
EFFECT: improvement in precision of target registering under the absence of direct sight of the target at the minimum consumption of ammunition and reduction of the risk for observer's life without use of optical instruments, sound and radar stations.
FIELD: weapons and ammunition.
SUBSTANCE: invention relates to onboard system of shooter detection, including several sensors attached to an aircraft shell, e.g. to a helicopter. Sensors detect only shockwave signals. Signals detected are analyser to locate a shooter with certainty. Analysis may include measurement of arrival time of missile shockwave at each sensor, obtainment of signal arrival time difference, calculation of ambiguous solution set corresponding to the shooter, and clustering the solution set to locate the shooter with certainty. Elliptic cluster is used.
EFFECT: possible increase of certainty of true shooter location detection.
4 cl, 8 dwg
FIELD: weapon and ammunition.
SUBSTANCE: method of automatic armaments homing at moving target according to which the periodic image of the field of military operations is formed with a frame frequency, and after target detection, determination of its range, speed of movement and an altitude the lead angles of the weapon for the subsequent shot, differs by that, for the purpose of increase of probability of target destruction and safety of a shooter, after detection of the target the shooter by means of remote control moves the target image to such area of the field of vision of the optical-electronic system (OES) of the sight which would allow at stable position of the line of vision (LV) of OES to observe the target during the time sufficient for the first aiming operation; at this operation the position of LV OES is stabilised spatially; the marker is placed over the image of OES target; the sight operating mode is switched to automatic one at which OES marker moves together with the target, and OES at the beginning of each shot transfers the data (an azimuth and a angle of a place) of the target angular coordinates to the range finder; the range finder is automatically rotated towards the coordinates supplied by OES and as the target enters the sight of the range finder marker it sends an impulse of radiation and determined the range of the target which it transmits to the sight, providing the first triad of data (location angle, an azimuth and range of the target) which are saved in the sight memory; after the time Δt0, multiple to the period of OES frame sweep, the range finder again measures the target range and again transfers the information on the target range to memory of the sight which automatically forms the second triad of data on the target position with reference to the sight; the calculator of the sight using both triads of data and the known time interval Δt0, predicts the target position at the given moment TP; and at calculation of TP the following is taken into account: target speed; range and angle of the target altitude; time of shell flight taking into account the target altitude; dynamic parameters of the sight drive (time of rotation of the sight to the rated point); size of differential coordinates of the second and first triads of data; ambient temperature; wind direction and speed; then LV OES stabilisation is removed and the sight with the weapon stock is rotated towards the direction of the predicted position; after installation of the sight into the rated position at the given time TP the shot is made automatically.
EFFECT: improvement of aiming accuracy taking into account parameters and target motion conditions, homing of the weapon to the rated direction with automatic providing the required lead angle, and the shot at the rated moment without participation of the shooter.
1 cl, 5 dwg
FIELD: weapon and ammunition.
SUBSTANCE: weapon unit with the aim device contains a bottom machine and a top machine on which a rotary cradle with the weapon and the parallelogram are installed on pins which consist of the machine bracket fixed with reference to the top machine, the lever connected with the cradle, rods and consoles with a land sight installed on it, an antiaircraft sight with a ring grid and an adjusting device for adjustment of vision axes of sights, the land sight is designed as a conic hollow bell extending by the front end towards muzzle part of the weapon and installed on the support by means of the rack, and the ring grid of the antiaircraft sight is installed coaxially to the bell of the land sight and by the internal ring is fixed at the back end face of the bell in such a way that the central projections of the external circle of the front end face of the bell and the external circle of the internal ring of the ring grid are visible from the centre of the structure located on the aiming line as a ring strip of identical width, the adjusting device it is designed as a bracket with bearing platforms on the ends interacting with reciprocal bearing platforms made on the support and the console of the parallelogram by means of adjusting and the fasteners having a possibility of axial movement. Fasteners are symmetrised around the adjusting elements. The ribs connecting raccourcir rings are implemented prominent inside the bell, on the bell end the aim level with the front sight in the bell centre of the aim device is located, holes in bearing platforms of the bracket are made with thread. The method of adjustment of the aim device of the weapon unit consists in adjustment of position of the weapon by combination of the axis of the stock channel of the weapon with the corresponding cross hairs of the reference target by means of the boresighting tube and alignment of the sight line of the aim device with the corresponding cross hairs of the reference target by means of the adjusting device. After adjustment of position of the weapon in the aim device the auxiliary bushing with longitudinal grooves is placed which is entirely implemented as a groove in the centre of the auxiliary bushing, and then backsight is aligned in the auxiliary bushing and the front sight of the aim level of the bell with the cross hairs of the reference target.
EFFECT: simplification of finding of necessary eye position providing an aiming, acceleration of aiming at the target, simplification of exact aiming at small or far targets, increase of vibrostability of fastening of the aim device, improvement of accuracy of adjustment of the aim device, acceleration of sight adjustment.
2 cl, 6 dwg
SUBSTANCE: method involves determination of a position and orientation of a freely moved instrument inside an aircraft. For that purpose, commands are supplied to emit pulse ultrasonic signals (UT) with emitters distributed along the instrument. Signals are received with UT receivers at distributed points on the instrument inside the aircraft. Moments of emission and reception of signals are synchronised via a radio channel. Temperatures are measured at arrangement points of UT emitters and UT receivers. As per this data and delay times of reception of signals, the above position and orientation of the instrument is determined. As per the current position of markers, turning angles of the instrument for its guidance to the same markers are calculated, and commands are generated for the instrument rotation. A guidance system includes required means for carrying out the above operations.
EFFECT: providing guaranteed guidance of an instrument freely moved relative to the instrument inside the aircraft to markers of any type.
2 cl, 1 dwg
SUBSTANCE: invention relates to AAGM and ATGM complexes, particularly to simulators for training operators of said complexes. IPU first set of I/O is connected with first set of I/O of operator's board. IPU second set of I/O and set of inputs are connected with actuator unit first set of I/O and set of inputs. Said actuator unit comprises minicomputer designed to generate simulation image, video converter to transmit image generated by said minicomputer to IPU, two microcontrollers for data exchange with combat vehicle and single-instruction unit top receive and to convert control commands from operator's board. Stabilised poser supply serves to feed minicomputer and actuator unit systems. Minicomputer incorporates the flash-memory card port. The latter serves to connect external devices to minicomputer. The latter with second set of I/O and set of inputs are connected to second set of I/O and set of inputs of combat vehicle operator board set of outputs. Board set of inputs makes the simulator first set of inputs.
EFFECT: improved training.
2 cl, 2 dwg, 2 ex
FIELD: weapons and ammunition.
SUBSTANCE: method for adjustment of barrel position during small arms firing includes target detection, arms aiming and shot initiation. Barrel position is adjusted vertically after target detection using thermal imager coordinated with arms and a sight. Thermal imager is mounted on arms displaying detected hot spot-target. Change of spot-target is controlled, primary signals from at least two first spots which detected hot target in sequence are processed. Shot is initiated by automatic impact by signal of control unit mounted on barrel of arms of device changing its position, mounted on arms in horizontal plane, connected to drive cinematically and to control unit electrically.
EFFECT: quick sighting and effective target damage.
12 cl, 11 dwg
FIELD: weapons and ammunition.
SUBSTANCE: invention refers to control of equipment of air defense rocket-cannon complexes. The control method of equipment of the air defense rocket-cannon complex involves detection and identification of a target, taking of firing decision and calculation of coordinates of a predicted collision point for firing by means of rocket and cannon equipment, guidance of equipment and rocket and/or shell firing, evaluation of firing results and taking decisions on firing continuation. At rocket firing, an aiming mark is aligned with the target by means of a sight; an air flow velocity is measured; angular corrections for deviation both of rocket and cannon equipment from a sighting line are determined considering firing conditions and ballistic characteristics of ejected rockets and shells, availability in the sight field of view of dust and smoke interference and their characteristics; the above corrections are entered to guidance actuators of the corresponding equipment; during flight of the guided rocket and after it is captured with a guidance system, in a number of the trajectory sections there performed is its deviation from the sighting line by correction of control commands of input of an additional constant signal and pseudorandom signals of a random number generator; besides, maximum level of corrected control commands and a deviation value of the rocket from the sighting line are restricted in a perspective plane perpendicular to the sighting line, and when the rocket approaches the target at the specified distance, correction of rocket control commands is stopped.
EFFECT: improving probability of target hitting and reducing probability of hitting of the guided rocket itself.
FIELD: weapons and ammunition.
SUBSTANCE: invention refers to military equipment. An optic system output is connected to an optic signal divider input, the output in spectrum range of 7-14 mcm and the output in spectrum range of 0.8-1.1 mcm of which are connected to inputs of a two-channel photoreceiving device. The first output of the two-channel photoreceiving device is connected to the first inertia detector and to the input of the first adder, and its second output is connected through an adjustable amplifier to the input of the second inertia detector and to the second input of the first adder. In addition, the device includes an output coincidence circuit and a detection radio channel that includes in-series connected transmitting-receiving antenna, transmitting-receiving microwave module with a modulating voltage generator, band-pass filter, amplitude detector, low-frequency filter, the third inertia detector, the second threshold device and the second comparator unit, the second input of which is connected through the second voltage divider to the output of the low-frequency filter. The output of the second comparator unit is connected to the second input of the output coincidence circuit, the first input of which is connected to the output of the first comparator unit.
EFFECT: improving detection accuracy of a target and interference immunity of the device.
FIELD: weapons and ammunition.
SUBSTANCE: actual shot result is assessed visually on shooting benches and platforms as per target hitting signs. The proposed method consists in the number of the following operations: sighting, distortion, aiming-off and letting-off. New features of the proposed method are that aiming-off is determined in advance and its values with a minus sign are entered to a sighting marker of video recorder on the weapon. At letting-off a signal is supplied from the trigger assembly to the video recorder, in which the corresponding image displays a hitting zone; then, shot result is analysed as per video record. In order to assess the shot result, it is enough to find a frame in the video record, on which shot debris are shown.
EFFECT: improving target hitting assessment accuracy and strike accuracy, and assessing actions of a shooter at target processing.
FIELD: weapons and ammunition.
SUBSTANCE: proposed method comprises carrier (off-highway vehicle, motorboat), automatic revolver self-loading grenade launcher differs in that carrier includes stationary hole to accommodate bullet-proof hemisphere with bracket (lever) arranged at swing or other support with low friction factor to receive grenade loaded launcher, its barrel being aligned with said bracket whereto attached is auxiliary weapon (antitank gun, machine gun). Their sights are pre-aligned with grenade launcher sight.
EFFECT: higher combat efficiency, lower losses.
4 cl, 1 dwg
FIELD: weapons and ammunition.
SUBSTANCE: in time interval between trigger release and fire spring release function of supervision of gun barrel position relative to target is transmitted to device whereat data received at trigger release and supervised contact of trigger and up to output of permit command by computer to supervisor. Data obtained at release of trigger target designator terminal is compared with that defined by computer as a target and is memorised as a reference data by data carrier. Results of said comparison are used to release or to inhibit permit signal to aforesaid supervisor. Note here that permit signal is output when gun barrel position with respect to target allows hitting the target. Fire spring is released after receipt of said permit signal.
EFFECT: higher accuracy of fire.
5 cl, 1 dwg
FIELD: applicable in instrument engineering, in particular, in instruments using remote control of the actions of the observer-operator on the ground.
SUBSTANCE: the method consists in measurement of the object coordinates, observer's coordinates and transmission of them for further use, as well as in finding of the observer's bearings with due account of obtaining of target designation and determination of the error of the preset and current coordinates. The observer performs scanning of the ground with fixation of the readings of the azimuth and elevation angle sensors, readings of the device for determination of the observer's own coordinates at detection by it of the object of observation. These data are transmitted to an individual control device of the observer. The own coordinates of each observer via individual transceivers are transmitted to the control and computations device of a group equipment, having a storage unit, which contains a digital model of the ground relief of observation and a data base for target distribution and renewal. The obtained data on location of the observers, as well as of the targets from the data base for target distribution are applied to the relief digital model. The data on the relative location of the observer and the target distributed to him are transmitted via the transceivers to the observer's control device, in which they are compared with the data obtained from the azimuth and elevation is transmitted to the indicators of the vertical and horizontal turning of the observer's scanning device. The device for finding one's bearings on the ground has location and orientation sensors, control and computations device, transceivers, scanning device for the observer with indicators of vertical and horizontal turning, sensors of the location in space in azimuth and angle of elevation, device for determination of the observer's own coordinates, having a navigational equipment linked with a satellite. The observer's transceiver is coupled to a group transceiving device connected to the control and computations device of the group equipment. The control and computations device of the group equipment comprises a storage unit, having a ground relief digital model and a data base for target distribution.
EFFECT: simplified and enhanced reliability of use of the system of transmission to the operator of the information on the direction on the ground.
3 cl, 2 dwg
FIELD: firing of artillery by shells with a time fuse in the flatland and mountain conditions.
SUBSTANCE: at determination of the correction to the time-fuse setting the distances between the observation point and the reference point, as well as between the observation point and the center of the group of air bursts are measured. The correction to the time-fuse setting is determined by the difference of the distances measured from the observation point to the reference point or target and to the center of the group of air bursts divided by the fuse correction scale equal to the change of the horizontal distance in meters at a change of the fuse setting by one division and multiplied by the cosine of the angle of correction for the offset.
EFFECT: enhanced accuracy, reduced time and simplified process of determination of the correction to the time-fuse setting.
FIELD: medical equipment.
SUBSTANCE: device has operator's control board, generators, power source, brightness changing unit, adders; lower frequency filter, cursor index lighting nit, light filters units, cursor index forming units, range finding units and so on as well as channels for bringing units into communication. Device also has program setting unit, scaling unit, switch which has first input connected with output of periodic signal frequency detector through scaling unit. Device has test showing manual control drive, integrator which has input connected with output of time interval detector. Device also has unit for finding average time of test right performance, additional operator's control board connected in series with random signal generator, program output unit which has second input connected with output of program setting unit, test showing unit which has second input connected with output of switch. Video control device has second and third outputs connected with second outputs of operator's additional control board and random signal generator correspondingly. Output of video control unit is connected with second input of unit for measuring average time for correct performance of test. Device provides 10-15% increase of operation of human operators.
EFFECT: widened functional capabilities; higher precision of estimation of psycho-physiological tiredness of operators; ability of correction of operator's condition.
FIELD: guided missile optical guidance systems, applicable in guided weapon systems with teleorientation in a laser beam.
SUBSTANCE: the optical sight of the guided missile guidance system has a coaxially installed sight and a projector including two injection lasers, whose emitting areas are positioned perpendicularly to the axes of the measured co-ordinates, system of laser emission ejection to a single optical axis, an optical scanner in the form of a rotating prism and a zoom lens installed in succession in this axis. The axis of prism rotation is matched with the lens optical axis. The sight has also a nontransparent shutter installed on the cell of the rotating prism, two optronic sensors fixed in parallel with one of the measured co-ordinates in the plane perpendicular to the projector optical axis, the angle between the lines connecting each sensor to the axis of rotation of the prism makes up 90 deg. The outputs of the first and second optronic sensors are connected respectively to the inputs of the first and second delay circuits, whose outputs are connected respectively to the first and second inputs of the exclusive OR circuit, as well as to the first and second inputs of the permanent storage, the output of the exclusive OR circuit is connected to the first inputs of the time counter of the channel switch. The output of the time counter is connected to the third input of the permanent storage, whose output is connected to the first input of the code-to-time converter, whose second input is connected to the output of the frequency standard and the second input of the time counter. The output of the code-to-time converter is connected to the second input of the channels switch, whose outputs are connected respectively to the inputs of the first and second lasers, use is made of the first and second pulse counters, whose first clock inputs are connected to the output of the frequency standard, the carry output of the first pulse counter is connected to the clearance input of the second pulse counter, whose information outputs are connected to the fourth input of the permanent storage.
EFFECT: enhanced range of guidance of the guided missile.
FIELD: means for measurement of psychological characteristics, in particular, devices for determination of the degree of eye fatigue at sighting of various objects.
SUBSTANCE: the device has an operator's control panel, optical forming system, the first and second control units, screening unit, series-connected power source, brightness variation unit, adder, low-frequency filter, sighting index illumination unit, light filters unit and a sighting index forming unit, as well as a generator of periodic signals with their adjustment unit, transducers and indicators of amplitude and frequency. The device has an additional screening unit, deviation sensor, light interference sensor, frequency comparison unit, and a unit for production of a point light source, and a drive of the pint light source with respective couplings.
EFFECT: enhanced truth of estimation of the state of operators.
FIELD: devices for sighting of various objects, for example, targets at firing.
SUBSTANCE: the device has an operator's control panel, optical forming system, first and second control units, screening unit, series-connected power supply source, brightness varying unit, adder, low-frequency filter, sighting index illumination unit, light filter unit and a sighting index forming unit, as well as a periodic signal generator with their adjustment unit, transducers and amplitude and frequency indicators. The device uses also an additional index forming unit, ammunition type transducer, transducer of ammunition initial distance from the target and a transducer of variation of this distance at movement of the carrier all connected to the first, second and third inputs respectively, index illumination frequency mismatch indicator, unit for input of images to the field of vision of the sighter-operator, whose first input is connected to the output of the additional index forming unit, and the second input-to the output of the index mismatch indicator. The introduced elements and couplings provide for expansion of the device functional potentialities, in particular, enhancing of the sighting accuracy, which makes it possible to enhance the device efficiency by 15 to 17%, and timely take the respective measures for correction of the characteristics both of the device and operators. Besides, opportunities are enhanced in estimation of the influence of various environmental conduits on the efficiency of operations of the sighting device and operators.
EFFECT: predicted variations of indications of the functional activity of the operator.
FIELD: safety means of passenger and passenger and freight aircraft.
SUBSTANCE: hi-jacking of an aircraft standing on the ground is prevented by detection of the terrorist and annihilation of him with the acid of small arms. Laying of the small arms an the terrorist is accomplished by computation of the terrorist location co-ordinates and the co-ordinates of the remote-controlled small arms and estimation of installation of the small arms. The terrorist is detected with the aid of at least one, controlled video camera installed in the aircraft cabin and connected via the an-board computer to the aircraft transmitter. The terrorist is annihilated by shooting from remote-controlled small arms through the aircraft skin with employment of the control computer.
EFFECT: enhanced accuracy of weapon laying on terrorists.
5 cl, 6 dwg
FIELD: armament and military equipment, in particular, fighting vehicle firing at a target, for example, with the aid of machine-gun (gun) mountings.
SUBSTANCE: according to the invention, range correction tables verified for the whole range of temperature and air pressure variation are calculated before firings. Approximating coefficients for pressure and temperature are selected. The target is detected and identified and taken for tracking. Kinematic corrections for motion of the target and carrier are determined. The dummy firing range with due account made for the temperature and air pressure deviation from the normal values is determined. Ballistic corrections: elevation and drift angles for obtaining the dummy range, correction for cross and range ballistic winds, for the parallax of the sight and gun or submachine gun mounting are determined. Simultaneously with the approximating coefficients for pressure and temperature the coefficient of mutual effect of pressure and temperature is selected. The range correction for the joint effect of pressure and temperature is determined and with due account made for it the total correction is determined at calculation of the dummy range. The barrels of the gun (machine gun) mount are constantly deflected relative to the sighting line with due account made for the corrections, and firing at the target is carried out.
EFFECT: enhanced efficiency of firing of the fighting vehicle due to the enhanced accuracy of fire.
4 cl, 10 dwg
FIELD: FOR TELEORIENTATION OF GUIDED OBJECTIVES, OPTICAL SIGHT OF GUIDED MISSILE GUIDANCE SYSTEM AND PULSE SHAPER.
FIELD: remote control of flight vehicles.
SUBSTANCE: the invention consists in bringing the searchlight emission in the sighting channel, formation of elision only at the moments when the time intervals between the pulses are equal to the reference values, visualization of the emission that has passed through the sighting channel. Besides, defection of the emission that has passed through the sighting channel. Besides, deflection of the searchlight optical flux in two mutually perpendicular directions is accomplished, which provides for alignment of the sight optical axis and the searchlight information axis. A rotary prism is introduced in the guidance optical sight, and the sighting channel is made on the basis of a TV camera, monitor, sighting mark forming unit, and a sighting mark position control panel. Two AMD circuits and a series-connected decoder and an OR circuit with respective couplings are introduced in the pulse shaper.
EFFECT: enhanced accuracy of guidance of the controlled objective.
4 cl, 4 dwg, 1 ex
FIELD: armament and military equipment, in particular, fire of fighting vehicle by rocket projectiles from sheltered fire positions.
SUBSTANCE: according to the obtained data on the position and type of separate targets from the composition of the multiple target, assigned consumption of projectiles, depending on the characteristics of the used ammunition, accuracies of account of meteorological and ballistic conditions of fire and determination of the co-ordinates of the separate targets and fighting vehicle, a symmetrical fire zone is assigned for each separate target, locating the aiming points so that the function of the fire density would have the maximum in the pointed with the co-ordinates of the given separate target. Then, the possible unifications of the aiming points, located in the zones of intersection of the fire zones of the separate targets are performed, the summary construction of projectiles is calculated so that the calculated so that the calculated and assigned constructions of projectiles would coincide, after that the multiple target is subjected to fire.
EFFECT: reduced construction of ammunition at a guaranteed level of probability of target destruction.
3 cl, 7 dwg