Abstract: A countermeasure arrangement including a countermeasure dispenser. An envelope at least partly encloses the countermeasure dispenser. A first control module is configured to control the countermeasure dispenser. A suspension module is arranged on the envelope for suspending the envelope on an aircraft. The suspension module has a form and a design that substantially correspond to the form and design of a suspension rail of a missile, so that the suspension module mates to a hard point on the aircraft, which is adapted to the missile.

Abstract: An amplifier stage in a radar system including an input matching stage, a transistor stage and an output matching stage. At least one of the matching stages includes a switch. Each switch is arranged to connect or disconnect a corresponding at least one grounded matching component to or from the matching stage. Each switch in the matching stages of the amplifier stage is a switch that is arranged to connect or disconnect grounded matching components to or from the matching stages.

Abstract: A method for validating received positional data in vehicle surveillance applications wherein vehicles transmit positional data indicating their own position to surrounding vehicles. A a radio direction finding antenna arrangement of a receiving unit receives a signal carrying positional data indicating an alleged position of a vehicle, transmitted from a radio source. The bearing from the receiving unit to the radio source is estimated utilizing the radio direction finding antenna arrangement and the received signal. The distance between the receiving unit and the radio source is estimated based on the time of flight for a signal travelling there between at known speed. An estimated position of the radio source is calculated based on the estimated bearing and the estimated distance. A deviation value indicating the deviation/coincidence between the alleged position of a vehicle is determined according to the received positional data and the estimated position of the radio source.

Abstract: A method, control module and system of a vehicle including at least a first and a second control computer each containing a number of local Digital Control Modules and at least one Actuator Control Module wherein the Actuator Control Module of each control computer is operatively connected to all local Digital Control Modules of the same control computer, wherein the Actuator Control Module of each control computer is further operatively connected to all Digital Control Modules of the electrical system in a manner that enables each Actuator Control Module of the system to receive internal data of each Digital Control Module of the electrical system.

Abstract: A method and apparatus for determining position and orientation enabling navigation of an object using image data from at least a first and a second 2D image from at least one camera mounted on said object. The method comprises the steps of: correcting images from one or several cameras and from at least a first and a second 2D image for their respective radial distortion and other measurable effects which result in poor image precision; matching 2D image items in and between at least a first and second 2D image; calculating a fundamental matrix by using correlated image points from at least a first and a second 2D image; calculating and extracting estimated first rotation and translation values from the fundamental matrix using single value decomposition (SVD) based on information from at least a first and a second 2D image; iterating more accurate final rotation and translation values by using the LevenBerg-Marquard algorithm and determining the position and orientation of said object.

Abstract: A range estimation device for use in an aerial platform including at least one passive sensor, a trajectory determination unit and a control system. A control unit is arranged to indicate to the control system to perform own-ship maneuvering of the aerial platform such that characteristics of passive sensor measurements from the at least one passive sensor enable a range estimation to a target to be determined. The control unit is arranged to determine characteristics of the own-ship maneuvering based on the range uncertainty estimations to the target. A method and a computer program product for use in range estimation device.

Abstract: The invention regards a plasma-enhanced active laminar flow actuator system (1) adapted to an aerodynamic surface (3) which has a nano-engineered composite material layer(5) comprising a set of electrodes arranged (7?, 7?) in at least an upper (P1) and a lower (P2) plane extending parallel with the aerodynamic surface (3); the electrodes (7?, 7?) comprising nano filaments (9); the electrodes (7?) of the upper plane (P1) are arranged in the aerodynamic surface (3) such that they define a smooth and hard aerodynamic surface (3);conductors (11, 11?) of nano filaments (9?) arranged for electrical communication between a control unit (13) and each of the electrodes (7?, 7?), wherein the control unit (13) is adapted to address current between cooperating electrodes (7?, 7?) of the upper and lower plane (P1, P2) from a current supply depending upon air flow characteristic signals fed from air flow sensor means (19).

Abstract: A method to minimize influence of interference sources by control of a signal to noise/interference ratio of a wideband antenna system connected to an electronic system. The wideband antenna system includes at least one array of at least two antenna elements/sub arrays. The signal to noise/interference ratio control includes establishing of cancellation directions for interfering frequencies in the antenna pattern in the direction of interference sources. The wideband antenna system is operational over a system bandwidth and operates with an instantaneous bandwidth. Estimation of interference source parameters is performed in an evaluation process. A wideband antenna system implementing the method.

Abstract: The invention relates to a training weapon system (1) intended for a recoilless antitank rifle (2), the training weapon system (1) comprising a sub-calibre barrel (3) for firing sub-calibre practice projectiles (4) provided with base plates (5), the sub-calibre barrel (3) being arranged in a shell-like body (6) in the barrel (7) of the recoilless antitank rifle (2), the front part of the sub-calibre barrel (3) being fitted in a guide part (8) for centring the barrel (3), and a rear part of the barrel (3) being fitted in a breech (9), comprising a firing channel (10) and a nozzle screw thread (11) for fitting a nozzle screw (12), which is arranged in the rear part of the shell-like body (6).

Abstract: Power supply arrangement for distribution of power from a DC power source having a positive terminal and a negative terminal to at least a first and a second DC power consumer, comprising: a first DC power consumer connected to said negative terminal of said DC power source by means of at least a first return line, a first DC-DC switching power converter connected to said first DC power consumer, and connected to said positive terminal of said DC power source, a second DC power consumer connected to said negative terminal of said DC power source by means of at least a second return line, a second DC-DC switching power converter connected to said second DC power consumer, and connected to said positive terminal of said DC power source, wherein a unit comprising a capacitor connected in parallel with an electrical device is arranged in each of said first and second return lines, wherein said electrical device has a diode function, whereby circulating ground loop currents are prevented.

Abstract: A method and apparatus for determining a position and attitude of at least one camera by calculating and extracting estimated rotation and translation values from an estimated fundamental matrix based on information from at least a first and second 2D image. Variable substitution is utilized to strengthen derivatives and provide a more rapid convergence. A solution is provided for solving position and orientation from correlated point features in images using a method that solves for both rotation and translation simultaneously.

Abstract: An arrangement for storing and launching payloads. An elongate body includes at least one launch opening. The elongate body is configured to store the payloads in compartments. The compartments include openings. The arrangement is configured to be mounted on a vehicle with a longitudinal direction of the elongate body essentially coinciding with a direction of motion of the vehicle. The elongate body includes deflectors configured to act on an air stream and to permanently create an air covering layer across and over the compartment openings during use.

Abstract: A system for facilitating autonomous landing of aerial vehicles on a surface. A beam emitter is directed downwards. A control module is configured to govern the vehicle. A processor processes image data. The beam emitter is arranged to emit simultaneously at least four beams directed towards the surface in order to project a pattern thereon. One beam emitter of the at least four beam emitters is placed in the center. An image capturing module captures subsequent images of the pattern.

Abstract: The invention pertains to a vehicle separation system for a plurality of vehicles wherein the system is arranged to cooperatively provide distance separation for the plurality of vehicles, the system comprising: a storage module arranged in each of the plurality of vehicles, wherein each storage module comprises information related to a reference trajectory for each of the plurality of vehicles, a deviation detection module arranged to detect a deviation from said reference trajectory and generate at least one deviation alert, a communication module arranged to communicate the at least one deviation alert to each of the plurality of vehicles in response to the detected deviation, a separation module arranged to calculate an update of the reference trajectory for at least one of the plurality of vehicles, based on the reference trajectory of each of the plurality of vehicles, in order to provide distance separation between the plurality of vehicles.

Abstract: A distributed power amplifier arranged to operate over a bandwidth. An input side with an input terminal is arranged to receive an input signal and connected to an input transmission line. An output side with an output terminal is adapted to deliver an output signal and connected to an output transmission line. A power splitter is connected to the input terminal, thus being arranged to divide the input signal in a first path to the input transmission line and in a second path to an input of an active matching circuit. The active matching circuit has an output connected to the output transmission line. The other end of the output transmission line is connected to the output terminal. A method to design a distributed power amplifier and to modify existing distributed power amplifiers.

Abstract: A distributed avionics system arranged in an aerial vehicle for controlling at least one avionics function. A plurality of avionics processing subsystems are interconnected in a network. Each avionics processing subsystem includes a processor arranged to process at least one task so as to provide a set of data messages including at least one unit of data related to controlling the at least one avionics function on basis of provided input data, related to conditions of the at least one avionics function. A memory module is in operative connection with the processor and is arranged to store instructions for the processor to process the at least one task. At least one of the avionics processing subsystems is arranged to transmit at least one synchronization cycle start signal onto the network.

Abstract: An aircraft article composite forming tool and a method for producing the tool. The aircraft article to be formed includes a composite material including an outer surface. The aircraft article composite forming tool includes a matrix laminate made of at least an upper ply including a forming surface for forming the aircraft article and outer surface. The upper ply includes a nano filament structure embedded therein.

Abstract: A method for suppressing repetition jammer signals and/or clutter signals by using a radar system wherein said radar system comprises, at least one wideband arbitrary waveform generator, for creating arbitrary waveforms, and at least one antenna operating with wide instantaneous bandwidth, enabling direction dependent waveform radiation, wherein said method comprises the steps of transmitting different waveforms in different directions; adapting transmitted waveforms in different directions depending on received waveforms such that a normalised signal to noise-jammer ratio, NSNJR, is maximized; and thereby providing received signals from repetition jammers and/or clutter that are substantially orthogonal to a received signal from a target; thereby achieving suppression of the repetition jammers and/or clutter.

Abstract: A method and apparatus for generating and optimizing a fundamental matrix for a first 2D image and a second 2D image to obtain the relative geometrical information between said two 2D images for points in the two 2D images that correspond to a mutual 3D point. According to the method, the geometrical projection errors in the correspondence points are used to select correct and accurate inliers. This method and apparatus provides a more accurate and precise fundamental matrix than conventional methods.

Abstract: The object of the present invention is to provide an inventive guidance system for tracking and guiding at least one object, wherein said guidance system comprises a base station (1) including an optical imaging system (3) configured to determine the angular position vector of said at least one object (5, 15), an optical communication link for transmitting guidance control commands from said base station (1) to said at least one object (5, 15), and steering means provided on said at least one object (5, 15) for adjusting the direction of said at least one object (5, 15) in response to said guidance control commands. The invention also provides a corresponding guiding method.