Abstract: A pile repair apparatus includes a metal clamp having left and right brackets connected by a hinge member. A friction surface is positioned along an inner surface of the metal clamp to improve the connection of the apparatus to a pile to be repaired. A platform is connected to a top surface of the metal clamp, and a means for providing buoyancy to the pile repair apparatus can be secured to the platform. The buoyancy of the apparatus allows a diver to move and to submerse the apparatus easily and to position the apparatus around a pile to be repaired by opening and closing the apparatus about the hinge member. The apparatus is secured to the pile by inserting a bolt through corresponding apertures in the left and right brackets of the apparatus.

Abstract: An intelligent electronic speed control (IESC) was developed that combines telemetry data from sensors on a small UAV with an intelligent rule set extracted from a trained artificial neural network (ANN) to detect and isolate faults and to predict future failures. IESCs integrated into the UAV's electronic architecture can serve to enhance UAV safety and reduce injury to personnel and damage to property by predicting failures and preventing accidents before they occur.

Abstract: A pile repair apparatus includes a metal clamp having left and right brackets connected by a hinge member. A friction surface is positioned along an inner surface of the metal clamp to improve the connection of the apparatus to a pile to be repaired. A platform is connected to a top surface of the metal clamp, and a means for providing buoyancy to the pile repair apparatus can be secured to the platform. The buoyancy of the apparatus allows a diver to move and to submerse the apparatus easily and to position the apparatus around a pile to be repaired by opening and closing the apparatus about the hinge member. The apparatus is secured to the pile by inserting a bolt through corresponding apertures in the left and right brackets of the apparatus.

Abstract: A pile repair apparatus includes a metal clamp having left and right brackets connected by a hinge member. A friction surface is positioned along an inner surface of the metal clamp to improve the connection of the apparatus to a pile to be repaired. A platform is connected to a top surface of the metal clamp, and a means for providing neutral buoyancy to the pile repair apparatus can be secured to the platform. The neutral buoyancy of the apparatus allows a diver to move and to submerse the apparatus easily and to position the apparatus around a pile to be repaired by opening and closing the apparatus about the hinge member. The apparatus is secured to the pile by inserting a bolt through corresponding apertures in the left and right brackets of the apparatus.

Abstract: An automatic unmanned aerial vehicle (UAV) flight control system for 3D aerial mapping includes a UAV with an onboard camera, and a controller capable of communication with a flight control module of the UAV. The controller is configured to determine an area mapping flight path based on terrain characteristics of an area to be mapped. The controller also can determine a structure mapping flight path based on the existence and location of vertical structures within the area to be mapped. The area mapping flight path can be appended with the structure mapping flight path, thus providing an integrated and optimized UAV flight path for 3D mapping and modeling.

Abstract: A pile repair apparatus includes a metal clamp having left and right brackets connected by a hinge member. A friction surface is positioned along an inner surface of the metal clamp to improve the connection of the apparatus to a pile to be repaired. A platform is connected to a top surface of the metal clamp, and a means for providing neutral buoyancy to the pile repair apparatus can be secured to the platform. The neutral buoyancy of the apparatus allows a diver to move and to submerse the apparatus easily and to position the apparatus around a pile to be repaired by opening and closing the apparatus about the hinge member. The apparatus is secured to the pile by inserting a bolt through corresponding apertures in the left and right brackets of the apparatus.

Abstract: An automatic unmanned aerial vehicle (UAV) flight control system for 3D aerial mapping includes a UAV with an onboard camera, and a controller capable of communication with a flight control module of the UAV. The controller is configured to determine an area mapping flight path based on terrain characteristics of an area to be mapped. The controller also can determine a structure mapping flight path based on the existence and location of vertical structures within the area to be mapped. The area mapping flight path can be appended with the structure mapping flight path, thus providing an integrated and optimized UAV flight path for 3D mapping and modeling.

Abstract: An embodiment of a high-mobility vehicle comprises a vehicle body, a track assembly attached to the vehicle body, arms pivotally attached to the vehicle body, and trackless drive wheels mounted on distal ends of the arms. Another embodiment of a high-mobility vehicle comprises a vehicle chassis, right and left drive motors attached to the vehicle chassis, right and left power transmission mechanisms having high torque and low torque sets of gears, track assemblies coupled to the high torque sets of gears, and trackless drive wheels coupled to the low torque sets of gears.

Abstract: A recoil mitigation apparatus for a projectile-firing device, such as an explosives disrupter, is provided. At least one brake shoe is positioned proximate the projectile-firing device and means are provided for urging the at least one brake shoe toward the projectile-firing device. The urging of the at least one brake shoe provides a frictional force to mitigate the recoil of the projectile-firing device. In a preferred embodiment, at least one pair of brake shoes are provided. In a further preferred embodiment, the each of the at least one pair of brake shoes are positioned in a facing, spaced apart relationship and the at least one pair of brake shoe combination is positioned in a coaxial relationship to the projectile-firing device.

Abstract: A braking system is provided for mitigating the linear or rotational motion of an object having an axis, the linear or rotational motion being coaxial with the axis. In particular, the motion is the type which is the result of an impulse imposed over a short period of time, typically less than one second. The object whose linear or rotational motion is to be mitigated is disposed coaxially within a tube. The braking system includes at least one brake shoe positioned within an annular free space defined by the outer surface of the object and the inner surface of the tube. The at least one break shoe may be urged against the outer surface of the object or the inner surface of the tube to effect the mitigation.

Abstract: A recoil mitigation apparatus for a projectile-firing device, such as an explosives disrupter, is provided. At least one brake shoe is positioned proximate the projectile-firing device and means are provided for urging the at least one brake shoe toward the projectile-firing device. The urging of the at least one brake shoe provides a frictional force to mitigate the recoil of the projectile-firing device. In a preferred embodiment, at least one pair of brake shoes are provided. In a further preferred embodiment, the each of the at least one pair of brake shoes are positioned in a facing, spaced apart relationship and the at least one pair of brake shoe combination is positioned in a coaxial relationship to the projectile-firing device.

Abstract: A braking system is provided for mitigating the linear or rotational motion of an object having an axis, the linear or rotational motion being coaxial with the axis. In particular, the motion is the type which is the result of an impulse imposed over a short period of time, typically less than one second. The object whose linear or rotational motion is to be mitigated is disposed coaxially within a tube. The braking system includes at least one brake shoe positioned within an annular free space defined by the outer surface of the object and the inner surface of the tube. The at least one break shoe may be urged against the outer surface of the object or the inner surface of the tube to effect the mitigation.

Abstract: An improved fluid container for the transport, collection, and dispensing of a sample fluid that maintains the fluid integrity relative to the conditions of the location at which it is taken. More specifically, the invention is a fluid sample transport container that utilizes a fitment for both penetrating and sealing a storage container under controlled conditions. Additionally, the invention allows for the periodic withdrawal of portions of the sample fluid without contamination or intermixing from the environment surrounding the sample container.

Abstract: A housing for the containment of instrumentation in a high pressure fluid environment that consists of a metallic endcap and ceramic cylinder bonded together. The improvement comprises a structure which results in the improved sealing of said housing as the fluid pressure increases. The cylindrical ceramic tube and endcap are dimensioned such that mechanical failure does not occur when exposed to the desired external operating pressures which includes up to 36,000 feet of water. The housing is designed to withstand the external operating pressures without being subject to mechanical failure or excessive deformation which results in the loss of pressure housing integrity via cracking or deformation of the ceramic tube, deformation of the endcap, or from failure of the bonding agent.

Abstract: An expendable oceanographic sensor apparatus is deployed from an airplane or a ship to make oceanographic observations in a profile of the surface-to-ocean floor, while deployed on the floor, and then a second profile when returning to the ocean surface. The device then records surface conditions until on-board batteries fail. All data collected is stored and then transmitted from the surface to either a satellite or other receiving station. The apparatus is provided with an anchor that causes descent to the ocean floor and then permits ascent when the anchor is released. Anchor release is predetermined by the occurrence of a pre-programmed event.