A gaseous matter capture system and method comprising an aerial unit configured to capture gaseous matter directly from the atmosphere and further comprising storage means configured to transfer said gaseous matter for further processing in a non-aerial unit for the purposes of climate change mitigation and further use of captured gases.

Correction management techniques are provided. In one embodiment, the techniques involve determining, via a first machine learning model, a first and second data based on a respective first and second raw data obtained from a plurality of sensors, determining, based on a deviation between the first data and the second data, an inaccuracy of the first data, identifying an ambient situation corresponding to the first raw data and the second raw data, selecting, from historical raw data of the plurality of sensors, a group of raw data corresponding to the ambient situation, and correcting, via a second machine learning model, the first data based on the selected group of raw data.

Embodiments include apparatus and methods for dispatching package delivery by aerial vehicles. The embodiments include a route module, a wind model, and a dispatcher. The route module is configured to generate a route for package delivery. The wind model configured to store wind factors associated with geographic areas and provide one or more wind factors associated with the route for package delivery. The dispatcher is configured to identify one or more aerial vehicles for assistance of package delivery in response to the one or more wind factors associated with the route and send a message to the one or more aerial vehicles.

Embodiments provide functionality to remotely observe atmospheric conditions. An embodiment, in response to receiving an indication of existence of an airborne aircraft, automatically selects an antenna from a plurality of fixed antennas based on a location and an orientation of each antenna of the plurality of fixed antennas. In turn, a request for data is sent to the aircraft using the selected antenna and, in response to the request, data is received from the aircraft. The data received from the aircraft is automatically processed in a manner determining an atmospheric condition.

Embodiments provide functionality to remotely observe atmospheric conditions. An embodiment, in response to receiving an indication of existence of an airborne aircraft, automatically selects an antenna from a plurality of fixed antennas based on a location and an orientation of each antenna of the plurality of fixed antennas. In turn, a request for data is sent to the aircraft using the selected antenna and, in response to the request, data is received from the aircraft. The data received from the aircraft is automatically processed in a manner determining an atmospheric condition.

An image processing device 100 includes a calculation unit 110 for calculating a solar radiation spectrum in a given area on the ground surface on the basis of an observed image of the area, a solar radiation spectrum component of the area, and the spectrum of a pure substance estimated in the area, and a conversion unit 120 for converting the observed image on the basis of the calculated solar radiation spectrum.

Embodiments provide in-flight configuration of satellite pathways to flexibly service terra-link and cross-link traffic in a constellation of non-processed satellites, for example, to facilitate flexible forward-channel and return-channel capacity in a satellite communications system. For example, each satellite in the constellation can include one or more dynamically configurable pathway, and switching and/or beamforming can be used to configure each pathway to be a forward-channel pathway or a return-channel pathway in each of a number of timeslots according to a pathway configuration schedule. At least some of the pathways can be further selectively configured, in each timeslot, to carry “terra-link” traffic to and/or from terrestrial terminals and “cross-link” traffic to and/or from one or more other satellites of the constellation.

Anemometer for independently measuring wind speed and direction in fluid medium. A second anemometer portion has at least one attribute resulting in different wind resistance in fluid medium than a first anemometer portion, such as a different: mass, shape, density, specific gravity, drag coefficient and/or freedom of motion. Different wind resistance causes inclination of anemometer when deployed to fall autonomously along a trajectory of fluid medium, where anemometer drag coefficient curtails initial ballistic trajectory such that anemometer enters free-fall descent after deployment. Anemometer includes inclinometer to obtain inclination measurements, and memory/transmitter to store/transmit inclination measurements. Local wind direction/speed is determined from inclination measurements based on direction/degree of anemometer inclination in correlation with measurement timings. Anemometer may be deployed from moving airborne platform. Anemometer may include conical second portion embedded into spherical first portion, where conical second portion has smaller mass and larger surface area than spherical first portion.

Aspects of the technology relate to an environmental sensor system that uses different types of detector units as part of an onboard lightning detection and evaluation system for a high altitude platform (HAP) operating in the stratosphere. These sensor suites may be employed with balloons and other high altitude platforms during operation in the stratosphere. Onboard data processing and analysis may be done either in real time or on stored data sets. The processing system can use the gathered sensor information to mitigate issues related to lightning-related transients. The information can also be used in route planning and real-time navigation of HAPs when hazardous conditions are detected. It can also be employed in a back-end control system for long-term route planning and fleet management.

Aspects of the technology relate to an environmental sensor system that uses different types of detector units as part of an onboard lightning detection and evaluation system for a high altitude platform (HAP) operating in the stratosphere. These sensor suites may be employed with balloons and other high altitude platforms during operation in the stratosphere. Onboard data processing and analysis may be done either in real time or on stored data sets. The processing system can use the gathered sensor information to mitigate issues related to lightning-related transients. The information can also be used in route planning and real-time navigation of HAPs when hazardous conditions are detected. It can also be employed in a back-end control system for long-term route planning and fleet management.