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65results about How to "Maximize collection" patented technology

Non-planar adaptive wing solar aircraft

A system and method for assembling and operating a solar powered aircraft, composed of one or more modular constituent wing panels. Each wing panel includes at least one hinge interface that is configured to rotationally interface with a complementary hinge interface on another wing panel. When a first and second wing panel are coupled together via the rotational interface, they can rotate with respect to each other within a predetermined angular range. The aircraft further comprises a control system that is configured to acquire aircraft operating information and atmospheric information and use the same alter the angle between the wing panels, even if there are multiple wing panels. One or more of the wing panels can include photovoltaic cells and / or solar thermal cells to convert solar radiation energy or solar heat energy into electricity, that can be used to power electric motors. Further, the control system is configured to alter an angle between a wing panel and the horizon, or the angle between wing panels, to maximize solar radiation energy and solar thermal energy collection. A tail assembly for the aircraft includes a rotational pivot that allows the flight control surfaces to rotate to different orientations to avoid or reduce flutter loads and to increase solar radiation energy and / or solar thermal energy collection from photovoltaic cells and / or solar thermal cells the can be located on the tail structure associated with the flight control surfaces.
Owner:AURORA FLIGHT SCI CORP

Resource allocation method in unmanned aerial vehicle auxiliary network based on wireless energy transmission

The invention discloses a resource allocation method in an unmanned aerial vehicle auxiliary network based on wireless energy transmission, and belongs to the field of mobile communication. The methodcomprises firstly, constructing an unmanned aerial vehicle auxiliary network scene composed of a base station, an unmanned aerial vehicle and a user; then separately constructing channel models and channel capacities between the user and the unmanned aerial vehicle and between the base station and the unmanned aerial vehicle; uing the transmitting power of the unmanned aerial vehicle to the userand the channel model between the base station and the unmanned aerial vehicle to construct and solve an unmanned aerial vehicle communication energy consumption model meeting a limiting condition, introducing a centroid concept to optimize the position of the unmanned aerial vehicle under the condition that a time distribution proportion and a power distribution proportion are given, continuously optimizing the time distribution proportion and the power distribution proportion under the condition that the position of the unmanned aerial vehicle is given, and alternately optimizing an optimalsolution; and deploying the unmanned aerial vehicle according to the optimal position of the unmanned aerial vehicle, and allocating wireless resources according to the solved optimal power and timedistribution proportion. According to the invention, the wireless energy is collected to the maximum extent while the requirement of user data rate is met, and the energy consumption is reduced.
Owner:BEIJING UNIV OF POSTS & TELECOMM

High-energy radiation scintillation detector comprising multiple semiconductor slabs

A multilayer semiconductor scintillator is disclosed for detection, energy quantification, and determination to source of high-energy radiation, such as gamma or X-ray photons or other particles that produce ionizing interaction in semiconductors. The basic embodiment of the inventive detector comprises a multiplicity of stacked direct-gap compound semiconductor wafers, such as InP and GaAs, each wafer heavily doped n-type so as to maximize its transparency to scintillating radiation. Each wafer is further endowed with surface means for detection of said scintillating radiation, such a hetero-epitaxial p-i-n photodiode. In a preferred embodiment, the photodiode layer in each wafer is pixellated so as to provide the x and y coordinates of an ionizing interaction event. Combined with the z coordinate provided by the wafer index in the stack, the inventive detector yields the three-dimensional coordinates of each ionizing interaction event associated with absorption of an individual quantum of high-energy radiation. This three-dimensional information enables a further disclosed advantageous analysis method that is suitable for rapid identification of radioactive isotopes and determination of the direction to the source of radiation.
Owner:KASTALSKY ALEXANDER +1

Cooperative active sensing method for rapid target searching of unmanned aerial vehicle (UAV) group

ActiveCN109947136ASolving Rapid Planning ProblemsSolving fast 3D trajectory planning problemsNavigational calculation instrumentsTarget-seeking controlFlight heightClosed loop
The invention discloses a cooperative active sensing method for rapid target searching of a UAV group, and belongs to the technical field of multi-UAV area monitoring. The method comprises that a target position is set according to a target monitoring area of the UAV group; a multi-UAV 3D trajectory plan is decoupled into plans in horizontal and vertical directions, the plan sequence in the horizontal direction of multi-UAV cooperative searching is determined on the basis of a tree-shaped dynamic increase self-organizing mapping algorithm, the flight height of the UAV group is adjusted, and all neighborhood of the target position is visited; a smooth closed-loop 3D trajectory plan of the UAV group is realized by means of a segmented smooth curve; and according to UAV path speed and acceleration constraints, a speed profile calculation is used to solve the problem in optimizing the shortest time of active sensing in the multi-UAV cooperative area. The processes are implemented simultaneously, more UAV can visit more target positions as possible within the shortest time according to the planed course, cooperative rapid target searching is realized, and an active sensing task is completed.
Owner:TSINGHUA UNIV

Method of operating a solar aircraft

A system and method for assembling and operating a solar powered aircraft, composed of one or more modular constituent wing panels. Each wing panel includes at least one hinge interface that is configured to rotationally interface with a complementary hinge interface on another wing panel. When a first and second wing panel are coupled together via the rotational interface, they can rotate with respect to each other within a predetermined angular range. The aircraft further comprises a control system that is configured to acquire aircraft operating information and atmospheric information and use the same alter the angle between the wing panels, even if there are multiple wing panels. One or more of the wing panels can include photovoltaic cells and / or solar thermal cells to convert solar radiation energy or solar heat energy into electricity, that can be used to power electric motors. Further, the control system is configured to alter an angle between a wing panel and the horizon, or the angle between wing panels, to maximize solar radiation energy and solar thermal energy collection. A tail assembly for the aircraft includes a rotational pivot that allows the flight control surfaces to rotate to different orientations to avoid or reduce flutter loads and to increase solar radiation energy and / or solar thermal energy collection from photovoltaic cells and / or solar thermal cells the can be located on the tail structure associated with the flight control surfaces.
Owner:AURORA FLIGHT SCI CORP
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