摘要:
A system is provided for guarding a perimeter, including a control center, a launch system, a controller and a communication system. The control center is configured for generating a control signal responsive to receiving infiltration information of an actual or suspected infiltration at a target zone associated with the perimeter by one or more infiltration agents. The launch system is configured for deploying one or more ready-to-launch UAV's to the target zone responsive to receiving the control signal from the control center. The controller is configured for operating the launched UAV(s) to home onto at least one such infiltration agent. The controller is also configured for identifying the nature of the infiltration agent or the nature of infiltration; and/or for tracking the infiltration agent via the UAV(s). The communication system is configured for providing data corresponding to the nature of the infiltration agent or the nature of infiltration, and/or for providing location data corresponding to the location of the infiltration agent being tracked by the UAV's to enable neutralization thereof. A corresponding method for guarding a perimeter is also provided.
摘要:
Ein batteriegespeistes Datenaufzeichnungsgerät für hohe mechanische Belastungen, insbesondere Beschleunigungen, ist beschrieben. Analogsignal (AI) oder digitale Daten (DI) werden über Wandler (103) oder (118) einem getakteten Controller (104) zugeführt und über diesen und einen RAM-Datenspeicher (105) an einer Schnittstelle (108) nach der dynamischen Beanspruchung ausgelesen. Eine erprobte Verwendung des Datenaufzeichnungsgeräts besteht bei der Forschung und Entwicklung von Munitionskörpern und deren Sicherheitssystemen; das Gerät wird nach dem Abschuss des Körpers geborgen und anschliessend werden die Daten ausgelesen.
摘要:
The invention relates to a launched aerial surveillance vehicle, more specifically to a grenade or under-slung grenade launcher(UGL) aerial surveillance vehicle, a surveillance system and methods of providing rapid aerial surveillance. The vehicle once deployed is capable of autonomous flight paths, with basic inputs to change the circular flight paths, so as to build up surveillance for an area of interest. The vehicle comprises at least on optical sensor, which may be IR or visible range, to survey the area of interest, and feed the images back to at least one remote user.
摘要:
Ein Verfahren zur Datenübertragung zwischen einer Basisstation (1) und einem zum Empfang der Daten bestimmten Flugkörper (11), der Teil einer Gruppe (10) von im Flug zu einem Zielgebiet (2) befindlichen Flugkörpern (11, 12, 13) ist und zu dem von der Basisstation (1) keine Sichtlinienverbindung besteht, weist die folgenden Schritte auf: a) Übertragen der Daten von der Basisstation (1) zu einem ersten Flugkörper (13) der Gruppe (10), zu dem von der Basisstation (1) Sichtlinienverbindung besteht, und b) Übertragen der Daten von diesem ersten Flugkörper (13) zu dem zum Empfang der Daten bestimmten Flugkörper (11).
摘要:
A surveillance vehicle (10) comprising a vessel (11) and a parasail (12). The vehicle (10) is loaded, in a pre-launch condition, into a mortar tube for projection therefrom towards an area of interest. In this pre-launch condition, the vessel (11) resembles a conventional mortar round and the parasail (12) is stowed within the vessel (11). Upon arrival at the area of interest, the parasail (12) is deployed from the vessel (11) and instrumentation collects survey data.
摘要:
The system comprises an attachment device (14) including a support structure (18, 20) and at least one band member (22) for releasably connecting the support structure (18, 20) to a load (12), such as a missile, carried by an aircraft, and an aerodynamic element (32) associated to the attachment device (14). The support structure (18, 20) of the attachment device (14) includes a support bracket (18) which is open upwards and an intermediate member (20) which is adapted to be attached to the support bracket (18) to close the support bracket (20) from above. The intermediate member (20) is arranged in the assembled condition between the instrument or apparatus (10) and the load (12). The aerodynamic element (32) is releasably attached to the load (12) in front of the instrument or apparatus (10).