Abstract: A manned vertical take-off and landing (VTOL) aerial vehicle comprises: a body comprising a cockpit having pilot-operable controls; a propulsion system carried by the body to propel the body during flight; a control system comprising a sensing system, a processor, and memory storing program instructions configured to cause the processor to determine a state estimate of the aerial vehicle within a region, a repulsion vector based on a repulsion potential field model of the region and the state estimate, and a collision avoidance velocity vector based on the repulsion vector and the state estimate; determine an input vector indicative of an intended angular velocity and an intended thrust of the vehicle based on pilot-operable control inputs; determine a control vector based on the collision avoidance velocity vector and the input vector; and control the propulsion system such that the manned VTOL aerial vehicle avoids an object in the region.

Abstract: Embodiments relate to data acquisition units or nodes and more specifically to seismic data acquisition units or nodes for use in data gathering for ambient noise tomography (ANT). Some embodiments relate to a method for data acquisition, and systems employing one or more data acquisition units. Some embodiments relate to systems comprising one or more satellites in communication with one or more data acquisition units for communication to a remote server, for remote storage, and processing for creating sub-surface tomography images accessible to client devices.

Abstract: A System including multiple data acquisition units. A data acquisition unit includes a housing whose interior volume is defined by an outer wall, a top part and a bottom part; the housing includes a geolocation unit for processing a time synchronisation signal, a data communication unit for enabling wireless data communication with an external gateway device, a processing unit, a geophone assembly in the housing to sense vibration received via a sensing probe, extending from the bottom part of the housing, and/or the housing and to generate output signals to the processing unit, and a power supply unit to supply power to the geolocation unit, the data communication unit and the processing unit; a geolocation antenna and a data communication antenna extending from the top part of the housing; the processing unit processes the output signals from the geophone assembly to determine an occurrence of a seismic event.

Abstract: Some embodiments relate to a manned vertical take-off and landing (VTOL) aerial vehicle (AV) and to methods relating to such VTOL AVs.

Abstract: Embodiments relate to data acquisition units or nodes and more specifically to seismic data acquisition units or nodes for use in data gathering for ambient noise tomography (ANT). Some embodiments relate to a method for data acquisition, and systems employing one or more data acquisition units. Some embodiments relate to systems comprising one or more satellites in communication with one or more data acquisition units for communication to a remote server, for remote storage, and processing for creating sub-surface tomography images accessible to client devices.

Abstract: Embodiments relate to data acquisition units or nodes and more specifically to seismic data acquisition units or nodes for use in data gathering for ambient noise tomography (ANT). Some embodiments relate to a method for data acquisition, and systems employing one or more data acquisition units. Some embodiments relate to systems comprising one or more satellites in communication with one or more data acquisition units for communication to a remote server, for remote storage, and processing for creating sub-surface tomography images accessible to client devices.

Abstract: Antennas suitable for deployment as part of a satellite, such as a low earth orbit (LEO) satellite. Some embodiments relate to antenna arrays for LEO satellites. An antenna, including a base; a first antenna patch body; and a second antenna patch body disposed substantially parallel to and spaced from the first antenna patch body; wherein the first and second antenna patch bodies are aligned along a central axis and coupled to the base; and wherein each of the first and second antenna patch bodies define surface corrugations.

Abstract: A low earth orbit (LEO) satellite including a processor, a memory, and a communication sub-system. The communication sub-system including: an antenna array and a reconfigurable digital logic processing device. The processor dynamically reconfigures the reconfigurable digital logic processing device to amplify or attenuate transmissions received from one or more directions of interest, or to amplify or attenuate signals transmitted by the antenna array in one or more directions of interest according to the orbital schedule of the LEO satellite.