230results about "Movable targets" patented technology

The invention belongs to the technical field of information, and discloses a subsonic target drone launch control method and system, and the method comprises the steps: obtaining target drone training task data, extracting specific scene parameters from task target diversity, and determining a launch trajectory configuration demand; analyzing the dynamic environment adaptation parameters according to a launching track configuration requirement to obtain a time sequence control precision requirement; a control instruction module is processed in an instruction combination mode, and an initial launching control strategy under the modular design capability is generated; for the initial launch control strategy, analyzing dynamic change in complex environment application, and judging a real-time adjustment strategy demand; if the real-time adjustment strategy requirement exists, flexible configuration of a control system is updated according to the dynamic environment adaptation parameters, and an adjusted launching track is obtained; and generating a target drone control scheme with an accurate training task through the adjusted launching track in combination with scene simulation effect data.

A shooting target launcher, associated components and methods. The launcher spins one or more helicopter-like shooting targets to launch the targets. A target connector receives the targets. The target connector is rotated about an axis of rotation to rotate the targets about the axis of rotation. The targets have fan blades that, when rotated, propel the target through the air.

A shooting target launcher, associated components and methods. The launcher spins one or more helicopter-like shooting targets to launch the targets. A target connector receives the targets. The target connector is rotated about an axis of rotation to rotate the targets about the axis of rotation. The targets have fan blades that, when rotated, propel the target through the air.

A target throwing machine includes a base and a turret surmounted by a throwing unit, the turret being movable in rotation relative to the base according to a main axis. The base includes an upper surface and the turret includes a lower surface opposite the upper surface. In which machine an intermediate system is interposed between the upper surface and the lower surface, the intermediate system being in contact with the upper surface and the lower surface and forming a sliding interface between the intermediate system and the upper surface and / or the lower surface.

The utility model discloses a high-speed large-maneuvering target drone, which relates to the field of unmanned aerial vehicles and comprises a drone body, wings, a horizontal tail, a vertical tail and an air inlet channel. The fuselage can reduce resistance to a great extent to realize high-speed flight; the wings adopt sweepback upper single wings to reduce the resistance during high-speed flight, the problem of overlarge transverse stability caused by sweepback and high placement of the wings can be avoided through the downward reverse design, and meanwhile, the wings can be integrally disassembled and assembled and have better operability and convenience; the control efficiency of a full-motion horizontal tail is high, and the heading stability under a large-angle-of-attack attitude can be improved through the design of the inverted-V-shaped tail; the vertical fin without the control surface can improve the course stability and ensure the matching property of the transverse course stability, and is light in structural weight and small in flight resistance; the bearing separation channel type air inlet channel can avoid landing damage of the air inlet channel in the parachute landing recovery process, and meanwhile the requirements for high total pressure recovery, low air inlet distortion, radar stealth and the like are met.

The invention discloses a man-machine interaction instruction generation method for target aircraft remote cooperative control, and relates to the technical field of man-machine interaction instruction generation. According to the method, a track prediction mechanism based on historical state data and a feedforward control strategy are fused, a response window of a control instruction can be judged in advance by constructing a short-time future state prediction sequence of a target drone, and the time sensitivity and the execution matching degree of the control instruction are greatly improved; structured instruction unit generation and multi-stage sub instruction chain analysis are adopted, so that the composite action is modularly expressed and finely disassembled, and the control precision and logic consistency of complex operation are effectively improved. Besides, by means of space attitude residual error screening, envelope boundary modeling and time tolerance design, a stable control area and a buffer area can be established in multiple directions, and the fault-tolerant capability and controllability in the high-dynamic flight state are improved.

The utility model provides a rail movable type multifunctional composite target drone, which relates to the technical field of target drone, and comprises a movable rail and a multifunctional movable composite target drone mechanism, and the upper side of the movable rail is provided with the multifunctional movable composite target drone mechanism. The multifunctional movable composite target drone mechanism comprises a main moving assembly, a traction assembly and an auxiliary moving assembly, and through the arrangement of the multifunctional movable composite target drone mechanism, a power motor is matched with a power gear through an external chain to drive a rotating rod and a power wheel to move, so that the rotating speed of the power wheel can be better controlled; different rotating speed requirements of users are met, the movement speed is more stable and controllable, a pushing spring can push a limiting wheel, the limiting wheel is clamped to the two sides of the inner wall of a moving rail, and therefore the vehicle head shell can move along the moving rail all the time, derailing is avoided, a lower supporting wheel can provide pulling force at the top end, and the vehicle head shell can move more stably. And after impact force of gun striking is received, the lower supporting wheels enable the headstock shell to be kept on the moving track.

A method for detecting a shot hit on an inflatable shooting target and for providing a real-time indication of the hit. The method includes the step of providing a shooting target system with one or more inflatable shooting targets, each of them is assembled on a blower, a power source that is connected to each blower through a controller that controls the activation of each blower, and a current meter between the controller and the power source. The method includes the second step of measuring the current that flow to a certain blower, detecting changes in the current level that occurs upon a hit in a certain inflatable shooting target that is assembled on that certain blower, and making and indication of the hit by turning off the certain blower or by sending a notification to a mobile device of the user or the operator.

This invention relates to a multi-functional target machine, belonging to the technical field of light weapons shooting training equipment. It includes a target surface, a transmission assembly, a rotation assembly, a tilting assembly, and a lifting assembly. The target surface is transmittedly connected to the rotation assembly, tilting assembly, and lifting assembly. The transmission assembly includes three sets of worm gear units driven by the same power source. The worms of the three sets of worm gear units are located on the same straight line. The power source can move along the straight line, and each movement drives only one set of worm gear units. The three sets of worm gear units are transmittedly connected to the rotation assembly, tilting assembly, and lifting assembly, respectively, realizing the rotation, tilting, and lifting operations of the target surface. This invention can solve the technical problems of existing multi-functional target machines, such as numerous drive motors, large drive component sizes, complex control, heavy weight, and low shooting training efficiency.

The invention provides an artificial intelligence confrontation technology military training simulation system based on reinforcement learning, and belongs to the field of training simulation. The problem of poor confrontation simulation training effect is solved; the scene simulation module is used for constructing a differential equation set and setting a response area of a target or a response interval of a laser module; the training simulation module is used for acquiring the positions of trainees, counting, recording and analyzing the shooting interval and the effective score of each trainee in combination with a differential equation set and the response area of the target or the response interval of the laser module, and adjusting a training strategy; the score feedback module is used for recording and feeding back effective scores of the trainees; the target refreshing interval and position are adjusted by analyzing the score and shooting angle of the trainee, and the target moving route is distributed according to the position of the trainee, so that the model effect of confrontation training is improved.

The utility model relates to a toy moving device. A shooting toy comprises the toy moving device. On the toy moving device, the driving mechanism drives the moving seat to move relative to the shell and is matched with the guide piece to slide along the guide track, linear motion of a single driving source is converted into rotating motion of the connecting arm, the problem that the manufacturing cost is increased due to a traditional multi-driving-source structure is solved, and therefore balance of function expansion and cost control is achieved. Secondly, through the sliding fit between the guide piece and the guide track on the shell and the rotary connection structure of the connecting arm on the movable seat, the shielding / opening action of the trigger piece and the displacement of the movable seat form linkage, the problem of space occupation caused by an additional transmission mechanism is solved, and therefore the composite motion function is achieved in the limited space; therefore, while the compactness of the product is ensured, the trigger piece can move relative to the shell along with the movable seat on one hand, and can be shielded / opened by the rotating connecting arm on the other hand.

The utility model provides a novel target throwing machine and a flying saucer shooting training system comprising the same, which solve the problems that the existing target throwing equipment cannot meet the requirements of throwing at different angles and at different heights and the like, and the main scheme is that the novel target throwing machine comprises a main machine, a target throwing plate, a saucer target and a target throwing arm, a transmission assembly is arranged in the main machine to drive the target throwing arm to rotate in a servo mode, the disc targets are stacked through a target frame, fall onto the target throwing plate from the bottom of the target frame and then are thrown out after being impacted by the target throwing arm, and the disc target throwing device is characterized in that a base plate is further arranged at the bottom of the main machine, and a rotating disc rotating in a servo mode is arranged at the top of the base plate. One end of the rotating disc is hinged to one side of the bottom of the main machine, an angle adjusting assembly is fixed to the other end of the rotating disc so as to adjust the elevation angle of the hinged position of the main machine, and the chassis can ascend and descend adjustably.

The utility model relates to the field of shooting targets, and provides a combined shooting target which comprises a stand column, a target seat, a target disc and an overturning target. The target seat is installed on the stand column. The target disc and the target head are detachably installed at the two ends of the target base respectively. The target disc is located in front of the stand column. The overturning target is located at the rear end of the stand column. According to the utility model, the upright post is punched, and the hexagonal bolt and the self-locking nut are used for fixing, so that the mounting height of the target seat can be freely adjusted according to different punching positions, the shooting requirements of different height positions can be met, and the application range is wide; meanwhile, the target disc and the target seat as well as the target head and the turnover target seat are connected completely through bolts and self-locking nuts, and no welding structure is needed, so that the target disc and the target head can replace target discs and target heads with different sizes and shapes at any time as required, the disassembly and assembly are more convenient, the application range is effectively expanded, the flexibility is higher, and the cost is lower. And different shooting requirements are effectively met.

This relates to biodegradable flying target compositions, biodegradable flying targets, and methods of manufacturing same. In one aspect, there is provided a biodegradable flying target composition comprising: a ground grain material having a granularity wherein about 90% to about 100% of the ground grain material will pass a mesh size of 0.15 and having a granularity wherein a majority of the ground grain material is incapable of germination or none of the ground grain material is capable of germination and having a moisture content of about 3% to about 21% by weight prior to molding into a flying target by application of heat and / or pressure. The disclosed solution comprises a biodegradable target formed from non-toxic materials that are wholly consumable by wildlife and farm animals without harm, thereby minimizing residual environmental impact.

Target device (100) for firing with long or short firearms, comprising at least one upright target (110) capable of withstanding firing with conventional hunting or sporting projectiles, characterized in that two targets (110, 120) are provided in pairs, which are coupled via a respective coupling device (111, 121) to a common rotatably mounted shaft (130), and the kinetic energy absorbed upon impact of a projectile on a first target (110) causes the first target (110) to be moved from a vertical position to a horizontal position by means of a rotation of the shaft (130) and simultaneously causes the second target (120) to be moved from a horizontal position to a vertical position by means of a rotation of the shaft (130).

Title: Target (1) for clay pigeon shooting, in the general shape of a dome having axial symmetry along an axis (z) and comprising a first convex face (10) comprising from the periphery, a skirt (101) then a tread (102) then a dome (100) having an envelope (110) which comprises at least one annular stage (120 a, b, c) centered on the axis z, each annular stage comprising a step (121a) and a riser (121b), characterized in that, for at least one annular stage, the riser comprises a plurality of cavities (131) and in that each cavity has a prism shape having two side walls (1312, 1312') connected to a transverse wall (1313) extending from a bottom wall (1311) along the axis (z). Figure for abstract: Fig.3.

Methods and apparatus for pointing logic in aircraft are disclosed. A disclosed example apparatus to aim an aiming device carried by an aircraft includes at least one memory, machine readable instructions, and processor circuitry. The processor is to at least one of instantiate or execute the machine readable instructions to determine a position of a target, determine an orientation of the aircraft, determine aiming points based on the orientation and a movement range of the aiming device, and determine a movement of at least one of the aircraft or the aiming device based on the aiming points and the position to orient the aiming device toward the target.

A system and method for recovery of undamaged frangible aerial targets at shooting ranges includes a net positioned horizontally above ground level to cover a target fall zone. The net has mesh openings sized to retain undamaged frangible aerial targets while allowing damaged targets to pass through. The net forms a closed loop around parallel elongated front and rear rollers supported above ground by a plurality of fixed caster assemblies. A motor operatively coupled to at least one roller drives the net in a conveyor-like motion. Undamaged targets landing on the net are transported by the net to a collection area positioned adjacent to the front roller. The system may include friction strips on the rollers to enhance traction and a protective barrier shielding the collection area from stray shotgun pellets, thereby enabling recovery and reuse of targets that would otherwise break upon ground impact.

A hidden display target based on illumination comprises a bottom plate, a light source, a supporting frame and a rotating disc, a plurality of inserting groove sets are sequentially formed in the middle of the bottom plate from the tail end to the front end, first inserting plates matched with the inserting groove sets are arranged at the bottom of the supporting frame, the first inserting plates of the supporting frame are inserted into the inserting groove sets, and the rotating disc is installed at the top of the supporting frame through a rotating shaft. A plurality of target-shaped hollowed-out parts are symmetrically distributed on the rotating disc with the rotating shaft as the center, an opening which does not shield the target-shaped hollowed-out parts is formed in the supporting frame to form a projection area, a limiting device capable of locking the rotating position of the rotating disc is further arranged on the supporting frame, and a light source is installed at the tail end of the bottom plate and is in a condensation light source form. The central axis of the light source coincides with the central axis of the target-shaped hollowed-out part in the projection area, and the distance between the light source and the rotating disc enables the light spot of the light source on the rotating disc to be larger than that of the target-shaped hollowed-out part. The device is reasonable in structure, practical in function, convenient to operate, low in cost and capable of powerfully improving the shooting training quality and efficiency.

The invention relates to a training system (1) for combating naval surface drones, this training system comprising: a remote operation system (2), a telecommunications system (3), one or more naval surface drones (5) which are configured to be operated simultaneously by the remote operation system (2), via the telecommunications system (3), to simulate an attack mission against one or more target ships (50), the number of naval surface drones (5) being in particular between 1 and 15, in particular between 3 and 10. Figure for the abstract: Fig. 1

To provide a technology that enables high-speed projection of target images.SOLUTION: As one of solutions, a target system comprises a target device having a screen, a first projector projecting a target on the screen and a control device controlling the first projector. The first projector comprises a light source of a single light, a condenser lens collecting an irradiated light of the light source, a projection lens and shadow picture forming means or a diffractive optical element provided in the projection lens that projects a target image onto the screen. The control device is configured to control ON / OFF of the light source.SELECTED DRAWING: Figure 4

The utility model discloses a horizontal motion target drone for shooting training, which comprises a bottom plate, the outer surface of the bottom plate is fixedly connected with a first motor, the output end of the first motor is fixedly connected with a screw rod, the outer surface of the screw rod is rotatably connected with a movable plate, the upper surface of the movable plate is fixedly connected with a fixed support, and the fixed support is fixedly connected with a fixed support. A movable target plate is arranged on the upper surface of the fixed support, a first open groove is formed in the bottom plate, and the lead screw is located in the first open groove; a supporting plate is fixedly connected to the upper surface of the bottom plate, a hydraulic push rod is fixedly connected to the outer surface of the supporting plate, a placing plate is fixedly connected to the upper surface of the hydraulic push rod, and a target showing and hiding plate is arranged on the upper surface of the placing plate. Through the components, the shooting precision and shooting accuracy of soldiers can be improved by arranging the movable target plate, and the shooting level of the soldiers is improved; and by arranging the display-hidden target plate and the shaking target plate, the response capability of soldiers is improved, and the functionality of the target drone is expanded.

The present invention discloses an image acquisition and processing device and a virtual-reality combined training system, which relate to the field of image acquisition and processing technology. This image acquisition and processing device includes a main body and a mounting seat, and the main body includes a shell, and also includes: an image acquisition module, which is arranged in the shell. This image acquisition and processing device and virtual-reality combined training system can seal and protect the human-shaped target to avoid the influence of impurities such as weeds and water stains. At the same time, it can clean the human-shaped target and exhaust the dust, which not only makes the clothes more tidy, but also makes the cleaning effect of the human-shaped target clothes better, ensuring its use effect and life; after receiving the electric signal of being hit, the sound and light alarm and the hollow cover can be moved to the highest position, and at the same time, the high-pressure air ejected from the blowing hole blows away the weeds and the like to avoid obstruction, and the high-pressure air blown out from the blowing pipe quickly blows the colored powder in the storage tank upward, so that the reminder effect is better, thereby improving the training effect.

The utility model discloses a kind of robot target machine of high-speed movement, it is related to robot target machine technical field, including robot platform and target body, the inside of the robot platform is provided with chamber, the downside of the robot platform is symmetrically provided with wheel, the inside of the chamber is provided with drive module, the side of the drive module is provided with power supply battery, positioning navigation module, environmental perception sensing module and robot control device, the drive module, positioning navigation module, environmental perception sensing module are electrically connected with robot control device, the top of the robot platform is provided with adjusting mechanism for adjusting target body position and direction. The utility model has multidimensional dynamic simulation ability, the robot target machine can be flexibly adjusted in horizontal, offset and vertical direction by the synergistic effect of adjusting mechanism, can simulate the complex motion trajectory of enemy target in actual combat, improve dynamic shooting ability.

The invention relates to an unmanned target aircraft wing with a high-lift airfoil profile and a diamond-shaped convex surface and a design method of the unmanned target aircraft wing. Comprising the following steps: designing and optimizing a high-lift airfoil profile of the unmanned target drone: defining basic parameters of the airfoil profile, establishing an airfoil profile parameterization formula, constructing an optimization model, and defining an optimization objective function, constraint conditions and decision variables; selecting an initial airfoil profile, giving initial design parameters, calculating aerodynamic characteristics, and solving an optimal value by adopting an interior point method to obtain an optimized airfoil profile; a micro vortex generator array is arranged on the surface of an unmanned target aircraft wing, and the layout and the structure of the micro vortex generator array are optimally designed; and obtaining the unmanned target aircraft wing comprising the high-lift airfoil profile and provided with the micro vortex generator array surface. The maximum lift coefficient is increased, the stall attack angle is increased, and the aerodynamic characteristics of the unmanned target drone are improved.

An entertainment system including at least one support pole, at least one attachment cord, a motor, wherein the motor is associated with the support pole and the attachment cord and a target, wherein the target is connected to the attachment cord, and wherein the motor is operable to cause the target to move in at least one of a vertical direction, a horizontal direction and a circular direction relative to the at least one support pole via the attachment cord.

A launching head for launching two or more sports shooting targets is provided, where each target is of a generally disc-shaped configuration. The launching head is of a generally tubular configuration defined by a longitudinally extending rotational axis and includes an outer circumferential support surface portion formed to fit into and support the respective targets. The launching head is provided with a plurality of retaining claw members configured to be able to pivot in a plane containing the longitudinal axis and pivot an angle relative to a plane extending perpendicularly to the longitudinal axis. A launching device applying the launching head to a sports shooting target is also provided.

A shooting target launcher, associated components and methods. The launcher spins one or more helicopter-like shooting targets to launch the targets. A target connector receives the targets. The target connector is rotated about an axis of rotation to rotate the targets about the axis of rotation. The targets have fan blades that, when rotated, propel the target through the air.

The utility model relates to the technical field of target shooting vehicles, in particular to a laser target shooting unmanned target vehicle which comprises a vehicle body, the vehicle body is a hollow rectangular cavity, a vehicle roof is arranged on the vehicle body, a supporting pipe is arranged on the vehicle roof, and a laser target plate is arranged on the supporting pipe. A moving track and a shaking plate are arranged on the outer walls of the two parallel sides of the vehicle body, the shaking plate is rotationally connected with the vehicle body, a boosting track is arranged on the shaking plate, the outline of the moving track is in a rounded rectangle shape, the outline of the boosting track is in a rounded triangle shape, and the shaking plate rotates to drive the vehicle body to shake up and down. Obstacle sensing assemblies are arranged on the outer walls of the other two sides of the vehicle body. The target vehicle is moved through cooperation of the moving track and the boosting track, and the shaking plate rotates and rolls to drive the vehicle body to shake in the moving process, so that the laser target plate shakes, and indoor simulation of a target vehicle cross-country scene is carried out.