296results about "Movable targets" patented technology

The invention relates to the technical field of stress calibration, in particular to a real-time feedback target drone dynamic stress calibration method and system, and the method comprises the steps: 1, dividing a dynamic stress sensitive region based on a target drone three-dimensional dynamic model; 2, original stress signals output by the multi-axis stress sensor array are synchronously collected, and preprocessed stress signals are generated; 3, inputting the preprocessed stress signal into a dynamic stress compensation model; and 4, in a target aircraft controlled loading test, comparing calibrated stress data with measurement data of reference measurement equipment, reversely correcting neural network weight parameters of the dynamic stress compensation model according to a comparison difference value, updating a weight distribution strategy of a weighted least square method, and completing dynamic iteration of calibration parameters. Through combination of the multi-axis stress sensor array and the dynamic stress compensation model, accurate measurement and compensation of the dynamic stress of the target drone are realized.

A toy launcher that can launch the flying rings over 100 feet with a more stable trajectory and more accurate trajectory based on the ring and blade configuration. The toy launcher includes a magazine assembly in which a plurality of the flying rings can be loaded in an axial direction, aligned with a launch direction. The rings are rotated up to speed and launched via movement of a sliding handle in a first direction, and the next ring in the magazine is advanced to the launch position by a return movement of the handle.

A live ammunition shooting competition system comprises a target area having a first and a second set of targets for a first and a second shooter, respectively. The first set of targets and the second set of targets are arranged such that the first shooter can view a shooting progress of the second shooter as the first shooter shoots at the first set of targets and the second shooter can view a shooting progress of the first shooter as the second shooter shoots at the second set of targets. A first computing device is associated with the first shooter and a second computing device is associated with the second shooter. Each of the first computing device and the second computing device is configured to allow the first shooter and the second shooter to challenge shooters to a shooting competition and to negotiate a parameter for the shooting competition.

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 handheld target thrower, components thereof, and associated methods. In some embodiments, the target thrower includes a frame, a thrower, and a target holder that holds the target in position to be thrown by the thrower when the thrower moves relative to the target holder. In some embodiments, the target thrower includes a firing mechanism including a release actuator and a safety spaced apart from one another such that both hands of an operator are required to fire a target. In some embodiments, the target thrower includes one or more debris outlets that allow debris, such as from broken targets, that may enter the target thrower to migrate out of the target thrower so as to not disrupt the operation of the target thrower.

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 utility model provides a remote intelligent control target, comprising a remote control console and an inflatable target terminal control system, wherein the remote control console comprises a mobile remote control console and a fixed remote control console; the inflatable target terminal control system comprises a fixed inflatable target terminal control system and a mobile inflatable target terminal control system, and the mobile remote control console cooperates with the mobile inflatable target terminal control system, and the fixed remote control console cooperates with the fixed inflatable target terminal control system, and the mobile inflatable target terminal control system comprises an inflatable target and a mobile carrier; a pressure reducing valve and an inflating valve are arranged on the inflatable target, and a fixed strap, a motor, wheels, and an inflatable target terminal controller are arranged on the mobile carrier, which has the advantages of not only achieving rapid installation and transportation of the target, but also reusing the gas supply accessories, effectively controlling the overall cost of the target, and making the whole system simple, cheap, and practical.

A collapsible, packable, and throwable aerial target of a disc-like shape, the aerial target comprising a circular body and an outer ring around periphery of the circular body, wherein the outer ring is in the form of a hollow tubular annulus that is divided into a plurality of sections, and each of the plurality of sections houses a plurality of pellets. The pellets are thoroughly filled in the outer ring sections to provide weight to the aerial target, but not overfilled to prevent flexibility, such that the aerial target can be folded and packed.

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 invention discloses a multi-mode hidden-display tactical target drone and a control system thereof, and relates to the technical field of shooting training equipment. A target drone main body is used for simulating a real target or an attack scene; the bullet point positioning system is used for detecting an impact signal when a bullet hits the target drone main body, and calculating and determining a bullet hitting position according to a data fusion algorithm and the impact signal; the multi-mode explicit-implicit control system is used for generating an explicit-implicit control instruction according to the bullet hit position, a preset explicit-implicit mode and a training requirement, controlling the target drone main body to perform explicit-implicit according to the explicit-implicit control instruction, and triggering a sound-light alarm; the wireless communication system is used for wireless communication among the target drone main body, the multi-mode hidden display control system and the control terminal; and the power management system is used for supplying power to the whole system and performing power management. According to the method, the hit detection precision is improved, multiple explicit and implicit control modes are provided, the training requirements of different shooting subjects can be met, and the authenticity and diversity of training are improved.

An open field game arrangement comprising a playing field including one or more unmanned vehicles that serve as ground or air targets, one or more display projectors that generate holographic targets, and a control system that determines whether a particular target was struck and generates one or more responses, such as a sound effect, a smoke effect, a scoring event, or other preprogrammed responses to a particular event.

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 discloses a target drone towed target releasing mechanism which comprises an installation connecting plate and a connecting bottom plate, two installation supporting arms are symmetrically arranged on the upper surface of the connecting bottom plate, a rotating connecting shaft is rotatably installed on the top between the two installation supporting arms, and a winding and unwinding disc is fixedly installed in the middle of the outer wall of the rotating connecting shaft. A traction steel wire rope is wound on the outer wall of the winding and unwinding disc, and a target body is fixedly installed at one end of the traction steel wire rope. The two ends of the rotating connecting shaft penetrate through the mounting supporting arms and extend outwards, and coil spring fixing cylinders are fixedly mounted at the extending ends of the rotating connecting shaft. According to the target drone dragging target releasing mechanism, through cooperation of the buffering coil spring, the brake, the brake disc and other structures, in the target main body releasing process, the direct impact force of the traction steel wire rope on the target drone is reduced, the speed of the target main body is gradually equal to that of the target drone, the stability and safety of the target drone in the navigation process are guaranteed, and the safety of the target drone is conveniently maintained.

The present application discloses a sealing structure for a target drone's water recovery equipment cabin, which relates to the field of target drones. The structure includes a groove provided in the circumference of an equipment cabin connection frame, an inflatable rubber tube is wound in the groove, an installation groove is provided through the equipment cabin connection frame, an inflatable tube port of the inflatable rubber tube is fixedly provided in the installation groove, and an auxiliary sealing structure is provided at one end of the inflatable tube port of the inflatable rubber tube away from the inflatable rubber tube, and the auxiliary sealing structure is used to seal the inflatable tube port. The present application improves the sealing performance of the equipment cabin by using an inflatable rubber tube in combination with a skin, while increasing the inflatable tube port, and uses an auxiliary sealing structure to seal the inflatable sealing tube, thereby effectively improving the long-term sealing performance of the inflatable rubber tube, and further improving the sealing performance and sealing time of the equipment cabin.

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.