Abstract: A method for remotely controlling an operated unmanned object, comprises defining of a set of control movements of an operator; selecting of minimal necessary signals to reliably acquire the operator's control movements; defining of a mapping of the control movements to commands for the operated unmanned object; sensing of operator's body movements; and transmitting of the minimal necessary signals corresponding to the operator's movements to the operated unmanned object.

Abstract: A device for electroadhesion and conversion of electrical energy into mechanical energy, for example electrostatic actuation, is provided, including a soft polymeric dielectric support having at least two sets of overlapping electrodes patterned respectively on the upper surface and bottom surface of the polymeric support, the electrodes of the two sets can be electrically activated through a power supply for providing voltage change suitable for electroadhesion, electrostatic actuation or both at the same time.

Abstract: A system for interacting with a remote object comprising a wearable jacket for a user, two actuators for supporting arms of the user, motors for causing movements to at least one of a torso and the arms of the user, and sensors for measuring at least one of a force applied to the user and a position of the user, and a controller and data transmission device for communicating with the remote object.

Abstract: A system for interacting with a remote object comprising a wearable jacket for a user, two actuators for supporting arms of the user, motors for causing movements to at least one of a torso and the arms of the user, and sensors for measuring at least one of a force applied to the user and a position of the user, and a controller and data transmission device for communicating with the remote object.

Abstract: An aerial vehicle, configured to transport cargo, and including a propulsion system and a foldable cage is described. The foldable cage is substantially linear while in a folded configuration, and substantially circular while in a deployed configuration. Moreover, the foldable cage includes a rods that form isosceles triangles. The rods are coupled together by flexible joints.

Abstract: A device for electroadhesion and conversion of electrical energy into mechanical energy, for example electrostatic actuation, is provided, including a soft polymeric dielectric support having at least two sets of overlapping electrodes patterned respectively on the upper surface and bottom surface of the polymeric support, the electrodes of the two sets can be electrically activated through a power supply for providing voltage change suitable for electroadhesion, electrostatic actuation or both at the same time.

Abstract: A variable stiffness device, including a core including a low melting point alloy, an encapsulation surrounding the core, the encapsulation made of an elastic material and sealing the core, and a heating device arranged around the encapsulation, configured to heat the core, wherein the elastic material of the encapsulation is subject to a tensile stress in a direction along a longitudinal extension of the thread-like variable stiffness device.

Abstract: A variable stiffness device, including a core including a low melting point alloy, an encapsulation surrounding the core, the encapsulation made of an elastic material and sealing the core, and a heating device arranged around the encapsulation, configured to heat the core, wherein the elastic material of the encapsulation is subject to a tensile stress in a direction along a longitudinal extension of the thread-like variable stiffness device.

Abstract: An aerial vehicle, configured to transport cargo, and including a propulsion system and a foldable cage is described. The foldable cage is substantially linear while in a folded configuration, and substantially circular while in a deployed configuration. Moreover, the foldable cage includes a rods that form isosceles triangles. The rods are coupled together by flexible joints.

Abstract: A VTOL (vertical take-off and landing) aerial flying vehicle comprising an inner frame, a gimbal system and an outer frame, the inner frame comprising a propulsion system and a control system. The propulsion system being able to generate a lift force. The control system being able to control the orientation of the inner frame. The gimbal system connecting the inner frame to the outer frame with at least two rotation axis allowing rotation freedom between the outer frame to rotate independently from the inner frame.

Abstract: An aerial vehicle including self-autonomous deployable arms and methods of deploying the vehicle are disclosed. The arms may include patterns located thereon that allow the arms to transition between wrapped, flat, and deployed configurations autonomously without the need for direct intervention by a user.

Abstract: An aerial vehicle including self-autonomous deployable arms and methods of deploying the vehicle are disclosed. The arms may include patterns located thereon that allow the arms to transition between wrapped, flat, and deployed configurations autonomously without the need for direct intervention by a user.

Abstract: A VTOL (vertical take-off and landing) aerial flying vehicle comprising an inner frame, a gimbal system and an outer frame, the inner frame comprising a propulsion system and a control system. The propulsion system being able to generate a lift force. The control system being able to control the orientation of the inner frame. The gimbal system connecting the inner frame to the outer frame with at least two rotation axis allowing rotation freedom between the outer frame to rotate independently from the inner frame.

Abstract: A new method for the estimation of ego-motion (the direction and amplitude of the velocity) of a mobile device comprising optic-flow and inertial sensors (hereinafter the apparatus). The velocity is expressed in the apparatus's reference frame, which is moving with the apparatus. The method relies on short-term inertial navigation and the direction of the translational optic-flow in order to estimate ego-motion, defined as the velocity estimate (that describes the speed amplitude and the direction of motion). A key characteristic of the invention is the use of optic-flow without the need for any kind of feature tracking. Moreover, the algorithm uses the direction of the optic-flow and does not need the amplitude, thanks to the fact that the scale of the velocity is solved by the use of inertial navigation and changes in direction of the apparatus.

Abstract: This present invention describes a novel vision-based control strategy for autonomous cruise flight in possibly cluttered environments such as—but not limited to—cities, forests, valleys, or mountains. The present invention is to provide an autopilot that relies exclusively on visual and gyroscopic information, with no requirement for explicit state estimation nor additional stabilisation mechanisms.

Abstract: A method for the genetic representation of a network (100), the network having one or more devices (20, 30, 70, 80), each device comprising at least one terminal (21, 22, 23; 71, 72) connected to at least one other terminal (21, 22, 23; 71, 72, 61) by a link with a value of interaction strength. The method includes associating with the devices terminal (21, 22, 23; 71, 72) a first sequence of characters (121, 122, 123; 171, 172), associating with the other terminal (21, 22, 23; 71, 72, 61) a second sequence of characters (121, 122, 123; 171, 172; 162), mapping at least part of the first sequence of characters (121, 122, 123; 171, 172) and at least part of the second sequence of characters (121, 122, 123; 171, 172; 161) to the value of interaction strength in order to determine the value of interaction strength.

Abstract: A method for the genetic representation of a network (100), the network having one or more devices (20, 30, 70, 80), each device comprising at least one terminal (21, 22, 23; 71, 72) connected to at least one other terminal (21, 22, 23; 71, 72, 61) by a link with a value of interaction strength. The method includes associating with the devices terminal (21, 22, 23; 71, 72) a first sequence of characters (121, 122, 123; 171, 172), associating with the other terminal (21, 22, 23; 71, 72, 61) a second sequence of characters (121, 122, 123; 171, 172; 162), mapping at least part of the first sequence of characters (121, 122, 123; 171, 172) and at least part of the second sequence of characters (121, 122, 123; 171, 172; 161) to the value of interaction strength in order to determine the value of interaction strength.