Abstract: Embodiments detailed herein relate to matrix operations. In particular, support for matrix (tile) addition, subtraction, and multiplication is described. For example, circuitry to support instructions for element-by-element matrix (tile) addition, subtraction, and multiplication are detailed. In some embodiments, for matrix (tile) addition, decode circuitry is to decode an instruction having fields for an opcode, a first source matrix operand identifier, a second source matrix operand identifier, and a destination matrix operand identifier; and execution circuitry is to execute the decoded instruction to, for each data element position of the identified first source matrix operand: add a first data value at that data element position to a second data value at a corresponding data element position of the identified second source matrix operand, and store a result of the addition into a corresponding data element position of the identified destination matrix operand.

Abstract: An active protection system for protecting a platform from an incoming threat. The system comprises: a detection system configured for providing an output data associated with an incoming threat; a first countermeasure arrangement mountable on the platform and configured to intercept an incoming threat at a far interception point; a second countermeasure arrangement mountable on the platform and configured to intercept an incoming threat at a near interception point; and a controlling unit, in communication with the detection system and with the first and second countermeasure arrangements, configured for receiving said output data and selecting a preferred countermeasure arrangement from said first and second countermeasure arrangements, with which the incoming threat is to be intercepted.

Abstract: A composite protective body suitable, among others, for making protective garments comprises a pliable flat case with at least one panel of soft ballistic material, and an insert within the case. The insert is composed of a plurality of consituent bodies of glass or ceramic material. The constituent bodies of the insert are of axisymmetrical or centrosymmetrical shape and of a size commensurate with that of the kinetic missiles against which protection is to be afforded. The bodies are arranged in at least two superimposed layers in each of which the constituent bodies are spaced from each other by a distance smaller than the size of a body with each body in one layer bridging a gap between two bodies of the adjacent layer. Each constituent body of the insert is glued to all surrounding bodies by thermoplastic or thermosetting material.