Abstract:
A system comprising an unmanned aerial vehicle (UAV) (100) configured to transition (520) from a terminal homing mode (510) to a target search mode (530), responsive to an uplink signal (451) and/or an autonomous determination of scene change.
Abstract:
The disclosed embodiments include a trailer for an autonomous vehicle controlled by a command and control interface. The trailer includes a trailer body configured to retain the autonomous vehicle in an undeployed configuration. The trailer also anchors the autonomous vehicle in a deployed configuration. A tether is provided having a first end coupled to the trailer body and a second end that is configured to couple to the autonomous vehicle. A winch is utilized to adjust a length of the tether to move the autonomous vehicle between the undeployed configuration and deployed configuration. Further, a communication system communicates with the command and control interface and the autonomous vehicle to control movement of the autonomous vehicle between the undeployed configuration and deployed configuration.
Abstract:
Remotely piloted aircraft or drone (1) adapted to induce artificial avalanche detachment, comprising: operating members (10) adapted to bring and/or keep said aircraft (1) in a flight condition; a cable (20) for connecting said aircraft (1) to an explosive charge (30) and holding said charge (30) suspended outside said aircraft (1); a triggering device (40) configured for causing the explosion of said charge (30).
Abstract:
There is disclosed an aircraft or aircraft section (1) having a bay formed therein, a bay door (3) for closing the bay, and locking means (4) for keeping the bay door in a substantially closed position. The locking means (4) are releasable during flight such that the bay door (3) is free to move between the closed position and an open position, subject to the flight configuration of the aircraft or aircraft section. A method of operating the bay door (3) is also disclosed.
Abstract:
In specific embodiments, a vehicle propellable through fluids or along surfaces, comprises a main work section and a plurality of propulsion units for propelling the main work section. The main work section supports one or more payloads. The propulsion units each include a rotor system and a ring-shaped wheel at least partially arranged about the rotor system and rotatable about the rotor system. The ring-shaped wheel is arranged at a banked angle relative to the rotor system.
Abstract:
L'invention a pour objet une munition 10 ou composant de munition comprenant une charge utile associée à une structure 2 d'emport de la charge utile, une partie au moins de la structure 2 étant réalisée en un matériau énergétique comprenant au moins un composant énergétique mélangé à au moins un premier matériau de renfort structural. La munition ou le composant comporte au moins un dispositif d'amorçage 24a, 24b de la structure énergétique 2, ledit dispositif étant relié à un moyen de commande 16, la structure constituant une enveloppe 12 délimitant une cavité 22 recevant un chargement 23 inerte ou pyrotechnique.
Abstract:
A suicidal explosion flight machine having a camera and a remote controller for the same are provided to permit a user to control the flight machine in a remote place such that the flight machine performs suicidal explosion when reaching a target point. A suicidal explosion flight machine includes a camera sensor(4), an explosion unit(13), a power supply unit(8) such as an electric motor having a battery or an engine having a fuel tank, a control board(10), and a flight servo mechanism and explosion controller(9). The explosion timing is controlled by a collision sensor or a remote controller.