Abstract:
Sistema aéreo remoto para medir variables ambientales en espacios cerrados y dispositivo aéreo remoto, para ser utilizado, por ejemplo, en invernaderos o instalaciones similares, y que comprende esencialmente el dispositivo (2) aéreo o estructura que vuela y una base (6) para recarga y estacionamiento. Asimismo, el dispositivo aéreo conformado por dicha estructura incorpora sensores de medición de variables ambientales y un sistema de navegación que no utiliza GPS, para poder ser utilizado en espacios interiores o cerrados. El dispositivo aéreo puede incorporar un globo o bolsa (3) de helio que sustenta la estructura en el aire.
Abstract:
Platform (100; 200, 200', 200") configured to acquire images and/or radio signals and to be carried by lightweight aviation aircrafts, characterised in that it comprises housing means (1, 3; 22, 201, 202, 203, 31) that houses one or more acquisition sensors selected from the group comprising or consisting of cameras (5; 51; 32) configured to acquire still and/or moving images and radio signal receivers (62; 34) configured to acquire radio signals, said housing means (1, 3; 22, 201, 202, 203, 31) being configured to be coupled to a light aviation aircraft (540), said one or more acquisition sensors (5; 51; 32; 62; 34) being connected to processing means (6; 23) configured to receive sensing data from a position and motion sensing unit (10; 230) coupled to said one or more acquisition sensors (5; 51; 32; 62; 34), said processing means (6; 23) being configured to control and/or program, on the basis of the received sensing data, each acquisition sensor (5; 51; 32; 62; 34) so as to enable the same to acquire images and/or radio signals when such acquisition sensor (5; 51; 32; 62; 34) is in a determined position and is subject to oscillations having a velocity that is not larger in absolute value than a maximum oscillation velocity value, whereby a rate of variation of an actual aiming of such acquisition sensor (5; 51; 32; 62; 34) is not larger in absolute value than a respective maximum value of rate of variation of offset with respect to an ideal aiming at a target, so as to ensure focusing of such acquisition sensor (5; 51; 32; 62; 34) on an aimed area.
Abstract:
A weather measurement system can include an aerial vehicle. An array of accelerometers can be disposed across the surface of the aerial vehicle. The accelerometers can be configured to measure raindrops impacting the surface. The measurements can include number per unit time and intensity. The system can include a processing unit configured to receive measurement data from the array and to process the measurement data into preprocessed data.
Abstract:
The present invention relates to a photographing and image acquisition system capable of switching a photographing mode for a meteorological target and efficiently acquiring an image. Particularly, an aspect of the present invention discloses a photographing and image acquisition system comprising a fixed camera mounted at the center of a flight vehicle; a rotary camera group composed of a left rotary camera installed on the left side of the fixed camera and a right rotary camera installed on the right side of the fixed camera; a mode switch control unit controlling a switch between multi-modes; and a stereogram performing unit making image data of an image acquisition region in a single mode into a three-dimensional image when an image acquisition region in a multi-mode partially covers the image acquisition region in the single mode.