1133results about "Movable targets" patented technology

A game operating device (controller) includes a longitudinal housing, and a holding portion held by hand to be wrapped by its palm it is formed in the housing. A direction switch is provided on an upper surface at a position where it can be operated by thumb of the hand holding the holding portion, and a start switch and a select switch are provided backward thereof. An X button 46 and a Y button are further arranged in line on the upper surface of the housing. An imaging information arithmetic unit is provided at a front end of the housing in a longitudinal direction in such a manner that an imaging device thereof is exposed from a front-end surface. A concave portion is formed on a lower surface at a position corresponding to the direction switch. The concave portion includes a valley and two inclined surfaces. An A button capable of being operated by index finger of the hand holding the holding portion is provided on the backward inclined surface. By processing an image signal obtained by imaging an infrared ray from LED modules by the imaging device, it is possible to obtain an operation signal varying according to a position and / or attitude of the controller.

Innovative new methods in connection with lighter-than-air (LTA) free floating platforms, of facilitating legal transmitter operation, platform flight termination when appropriate, environmentally acceptable landing, and recovery of these devices are provided. The new systems and methods relate to rise rate control, geo-location from a LTA platform including landed payload and ground-based vehicle locations, and steerable recovery systems.

A game apparatus is capable of controlling infrared radiation means for radiating infrared light. The game apparatus executes game processing using imaging information on the infrared light obtained from an input device. The input device takes an image of the infrared light radiated by the infrared radiation means, and also receives an input from a user. The game apparatus comprises pattern storage means; selection means; and radiation control means. The pattern storage means stores at least one signal pattern of an infrared signal usable by a control target device. The selection means selects at least one of the at least one signal pattern stored by the pattern storage means, using the input received by the input device. The radiation control means causes the infrared radiation means to output an infrared signal of the signal pattern selected by the selection means.

A firearm laser training system according to the present invention includes a laser assembly, actuable target assemblies and a computer system. The laser assembly is attached to a user firearm to project a laser beam toward the target. The target assemblies raise and lower targets in accordance with control signals from the computer system. Targets are raised to indicate intended targets, and are lowered in response to the beam impacting the raised targets or upon expiration of an interval without a beam impact. A corresponding target assembly forwards information to the computer system for display via wired or wireless communications. In addition, the training system may employ stationary target assemblies and / or laser-detecting body gear worn by exercise participants. The target assemblies and body gear communicate impact information to the computer system via wireless communications and may be utilized to create various training scenarios for firearm training.

A sports simulation system includes a projectile tracking apparatus having a display surface on which a visually apparent three-dimensional sports scene is presented. The projectile tracking apparatus captures images of a projectile tracking region disposed in front of the display surface to detect a launched projectile traveling through the projectile tracking region towards the display surface. At least one processing stage communicates with the projectile tracking apparatus and is responsive to the image data to determine the three-dimensional positions, velocity and deceleration / acceleration of a detected projectile traveling through the projectile tracking region. The determined three-dimensional positions, velocity and deceleration / acceleration are used by the at least one processing stage to calculate a trajectory of the launched projectile into the visually apparent three-dimensional sports scene. Updated image data is generated by the at least one processing stage that includes a simulation of the launched projectile into the visually apparent three-dimensional sports scene following the calculated trajectory. A display device coupled to the at least one processing stage receives the image data from the at least one processing stage and presents the visually apparent three-dimensional sports scene, including the simulation, on the display surface.

A method, apparatus, and program for computing a path, starting velocity, aim angle, and aim points for directing a putted golf ball from a point on a golf course to another point and incorporating such data into easily read charts or electronic media is provided. The invention also provides a means of determining the initial launch conditions and actual path a putted golf ball traveled on given its starting and ending ball positions.

The author suggests a new method and a new inexpensive, large blade-rope type wind rotor, that will be suspended at high altitude and produce huge quantities of energy. The air installation embodiment includes (FIG. 25): propeller 220, wing 226, rope transmission 229, electric generator 12 located at ground. Water rotors can utilize energy of ocean and sea streams. The invention contains 11 projects: 6 for air, 1 for a river, 3 for the sea and ocean, and 1 for ships. They have a power capacity of up to 60 MgW (air), up to 200 MgW (water) for one unit. The suggested installations have the following advantages: 1. Huge power production capacity-up to 5000-10000 times more than conventional ground-based rotor designs. 2. The rotor operates at high altitude of 1-14 kilometers, where wind has high speed and high stability (permanent flows). 3. The installation is much less expensive compared to conventional currently-employed windmills, partly because no tower is necessary to fix the rotor in space. 4. Wind energy is free -environmentally friendly.

An aerostat assembly, specifically an aerostat assembly including one or more cameras for aerial photography and surveillance. The aerostat assembly includes a frame assembly having a pivot assembly joined to a balloon tether line. Thrusters on the frame allow an operator to maneuver the assembly to desired positions as well as rotate the frame assembly about the pivot assembly.

An unmanned, towable aerovehicle is described and includes a container or frame to hold or support cargo, at least one and, in some examples, a plurality of autogyro assemblies connected to the container and to provide flight characteristics, and a controller to control operation the autogyro assembly for unmanned flight. The container or frame includes a connection to connect to a powered aircraft to provide forward motive force to power the autogyro assembly. In an example, the autogyro assembly includes a mast extending from the container, a rotatable hub on an end of the mast, and a plurality of blades connected to the hub for rotation to provide lift to the vehicle. In an example, an electrical motor rotates the blades prior to lift off to assist in take off. In an example, the electrical motor does not have enough power to sustain flight of the vehicle. The aerovehicle can further include plurality of autogyro assemblies to assist in flight. The aerovehicle can include surfaces that provide lift or control to assist in the flight profile of the aerovehicle.

A resettable target is provided with pivotable targets that rotate from a downward position to an upward position and are reset by reverse rotation when momentum is transmitted from a projectile to a reset target.

Embodiments of the present invention relate to concentrating solar radiation using an assembly of at least one clear and one reflective film that inflates into a shape reflecting parallel rays of light to a concentrated focus in the interior or immediate proximity of the assembly. Embodiments of the present invention can be assembled in a substantially flat stack with bonds or welds between the films, compatible with conventional high-throughput film manufacturing processes. Embodiments in accordance with the present invention may employ external circumferential rings or a “harness” assembly to support and point the balloon against wind forces and the like without severe stress localization. Embodiments in accordance with the present invention may also employ film attachments to facilitate feedthroughs, reduce stress concentrations, and modify the inflated shape. Embodiments in accordance with the present invention may also employ film modifiers, including laminated films, adhesives, printing, etc. to facilitate installation, feedthroughs, and other functions.

A high-altitude unmanned stratosphere aerial vehicle includes a fuselage, wings, control surfaces, and a propulsion system including an engine and a propeller. Each wing has a plurality of hoses and wing spars extending in a direction perpendicularly to the longitudinal fuselage axis and are surrounded by a skin forming a wing covering that determines the cross-sectional contour of the wing, the cross-sectional contour forming a laminar flow airfoil that generates high lift when there is low flow resistance. At the free end facing away from the fuselage, each wing has a winglet extending transversely to the longitudinal wing axis. The winglet has a movable control surface, which allows an aerodynamic side force to be generated so as to bring the aerial vehicle to a banked position.

A system and method are provided for using a first aircraft to retrieve a second aircraft. The first aircraft is typically larger than the second aircraft. A minimum airspeed of the first aircraft is typically greater than a maximum airspeed of the second aircraft. The first aircraft flies in a substantially circular pattern and extends a tow line, such that the tow line forms a substantially helical shape behind and below the first aircraft. Due to the helical shape, there is at least one point along the extended tow line at which the speed of the tow line is substantially equal to the speed of the second aircraft. The second aircraft can readily latch onto the tow line at that point, thereby minimizing potential damage otherwise caused by differential airspeeds.

A system is disclosed whereby a sensor, communication device, or other payload may be lofted to an operational altitude and maintained over an area of interest for some time by a relatively inexpensive and disposable buoyant aircraft, then returned intact to its point of origin or another desired location by a reusable but also relatively inexpensive non-buoyant aircraft. Automatic unpiloted control is used for all stages of flight, including ascent, loiter, return, and landing Specialized equipment can be provided to simplify launch procedures, reducing the number of personnel required to operate the system.

A firearm training system provides a firearm body having a trigger and a trigger pull sensor circuit. When the trigger is pulled, the trigger pull sensor circuit provides trigger pull data allowing monitoring of the actual two-dimensional trigger pull path taken by the trigger during the trigger pull. The trigger pull path is graft on a predetermined map together with boundary lines representing a predetermined difference threshold from ideal trigger pull data. The system provides a way to monitor trigger pull path to determine whether the trigger has been pulled laterally and / or the firearm body has moved with respect to a longitudinal axis of the firearm body during the trigger pull. By repeatedly monitoring trigger pulls using the system, a user can train to improve trigger pull technique.

Gaming utilizing actual telemetry data. In one embodiment, a system including a source of actual telemetry data regarding an event, such as a sporting event, and a gaming application utilizing the actual telemetry data. In one embodiment, by utilizing actual telemetry data, the ability to play a game as if the game player were involved in a current sporting event, in real-time, is provided.

An airborne surveillance platform supporting optoelectronic and electronic sensors, including level sensors, is automatically stabilized in a horizontal plane by varying the length of two tethers out of three. Error signals from the level sensors are transmitted over a wireless link to control components on a rotating platform on the host vehicle, which automatically vary the length of tethers. Applications include images of the surrounding terrain generated by a video camera and a thermal imager in military, police and civil emergency operations.

An annular protective rim attachment designed to grip the outer peripheral edge of compact discs (CD's) and digital video discs (DVD's), consisting of a flexible, flat top rim (10), the inner periphery of which is molded to form an upper lip (12), lower lip (14), and between these lips, a gripping mouth (16) to securely hold the CD or DVD (28) inside the aperture of said ring. The underside of said ring is shaped in such a way as to create an airfoil (20) adequate to enable the airfoil ring with attached CD or DVD (28) to safely fly and exhibit controllability when tossed into the air. The airfoil ring is made of a soft, flexible non-malleable plastic material which will create a cushioning effect so as not to produce contact impact and resultant injury or damage when tossed into the air.

A system is disclosed whereby a sensor, communication device, or other payload may be lofted to an operational altitude and maintained over an area of interest for some time by a relatively inexpensive and disposable buoyant aircraft, then returned intact to its point of origin or another desired location by a reusable but also relatively inexpensive non-buoyant aircraft. Automatic unpiloted control is used for all stages of flight, including ascent, loiter, return, and landing Specialized equipment can be provided to simplify launch procedures, reducing the number of personnel required to operate the system.

A goal for a collapsible, three-dimensional game includes: (a) at least two generally ring-shaped, openable hoops, each of the hoops being openable, closable, and coupleable at a hoop coupling of each hoop, the hoops including at least three post connecting mechanisms; (b) at least three detachable posts of substantially equal length, the posts being removably connectable to one of the post connecting mechanisms on the hoops; (c) a substantially flexible net affixed to an upper one of the hoops; and (d) a detachable net holding mechanism attachable to the post connecting mechanisms on each post; wherein, when the goal is in an open, erect position: a lower one of the hoops rests on the playing surface, the upper hoop being substantially parallel to and spaced apart from the lower one of the hoops, the net extending downwardly between the substantially horizontally oriented hoops.

A game apparatus selects one of a plurality of characters as a selected character. The game apparatus also sets a position of a virtual camera in accordance with the position of the selected character and thus causes a display apparatus to display an image of a game space, and also causes the display apparatus to display a cursor for designating a predetermined position in the game space. When a predetermined operation by the player is performed in the state where one of the non-selected characters is designated by the cursor, the game apparatus sets the non-selected character designated by the cursor as a newly selected character. When the selected character is changed in a first change step, the position of the virtual camera is moved in accordance with the position of the newly selected character.

Systems and / or methods for forming a multiple-articulated flying system (skybase) having a high aspect ratio wing platform, operable to loiter over an area of interest at a high altitude are provided. In certain exemplary embodiments, autonomous modular flyers join together in a wingtip-to-wingtip manner. Such modular flyers may derive their power from insolation. The autonomous flyers may include sensors which operate individually, or collectively after a skybase is formed. The skybase preferably may be aggregated, disaggregated, and / or re-aggregated as called for by the prevailing conditions. Thus, it may be possible to provide a “forever-on-station” aircraft.

A small arms training target system including a portable, battery powered, rail guided, motor driven carriage, with stationary and moving targets connected thereto. A target-rotate control device operatively connects an electric motor and rotational arm assembly to rotate and position the target into and out of a field of view. The position is selectable by a remote control, pre-selected program, or when a sensor attached to the target is struck by a sensor. Additionally an obscuring medium is attached to the rotational arm, with a target, having on it an image of a weapon mounted behind the obscuring medium. The position of the obscuring medium is selectable to be in front of the image of a weapon, making the target a no-threat, or not in front of the target, making it a threat.

A device to provide control of the trajectory of a lighter than air vehicle, such as a balloon, is provided. A lifting device, such as a wing on end, is suspended on a tether well below the balloon to take advantage of the natural variation in winds at different altitudes. The wing can generate a horizontal lift force that can be directed over a wide range of angles. This force is transmitted to the balloon by the tether. Due to this force, the balloon's path is altered depending on the relative sizes of the balloon and the wing. A relatively small amount of power is needed to control the system, possibly with a rudder. As the energy of the wind provides most of the force, the wind's energy does most of the work. The balloon is able to avoid hazards, to reach desired targets, to select convenient landing zones, and to provide other operational advantages. As a result, fewer flights must be terminated early due to an inability to control the trajectory, and it is easier to obtain permission to launch since a planned flight path can be achieved within a greater range of conditions.