METHOD observation of objects with remote controlled aircraft, remotely piloted aircraft and review personnel system remotely piloted AIRCRAFT

摘要

1.method u043du0430u0431u043bu044eu0434u0435u043du0438u00a0 objects with remotely manned aircraft u0437u0430u043au043bu044eu0447u0430u044eu0449u0438u0439u0441u00a0 is watching the image transmitted from the u0434u0438u0441u0442u0430u043du0446u0438u043eu043du043d the manned aircraft in the current time, u043eu0441u0443u0449u0435u0441u0442u0432u043bu00a0u044eu0442 search, detection and recognition of objects in the process of u043du0430u0431u043bu044eu0434u0435u043du0438u00a0 will staff the u043bu0435u0432u0438u0437u0438u043eu043du043du044bu0435 (infrared) camera with various u043fu043eu043bu00a0u043cu0438 u0437u0440u0435u043du0438u00a0, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 orderobservation u043eu0441u0443u0449u0435u0441u0442u0432u043bu00a0u044eu0442 by personnel review system, u0441u043eu0441u0442u043eu00a0u0449u0435u0439 from several cameras with u043du0435u043au043eu043bu043bu0438u043du0435u0430u0440u043du044bu043cu0438 located in a vertical plane u043eu043fu0442u0438u0447 u0435u0441u043au0438u043cu0438 u043eu0441u00a0u043cu0438, u0443u043fu0440u0430u0432u043bu00a0u044eu0442 aircraft at a rate u0443u0434u0435u0440u0436u0438u0432u0430u00a0 image object on the vertical central line of the frame.in the transition u0438u0437u043eu0431u0440u0430u0436u0435u043du0438u00a0 object from u043fu043eu043bu00a0 u0437u0440u0435u043du0438u00a0 one camera in the field and subsequent cell u043eu0441u0443u0449u0435u0441u0442u0432u043bu00a0u044eu0442 switching chambers and in the case of a u0438u0437u043eu0431u0440u0430u0436u0435u043du0438u00a0 the object in the field u0437u0440u0435u043du0438u00a0 cells with the most narrow field u0437u0440u0435u043du0438u00a0 memorise the frame, after which the status of u0438u0437u043eu0431u0440u0430u0436u0435u043du0438u00a0 u0437u0430u043fu043eu043cu043du0435u043du043du043eu043c object in the frame.the coordinates and angles of orientation of remote manned aircraft u0432u044bu0447u0438u0441u043bu00a0u044eu0442 coordinates of the object.;2.remotely manned aircraft, which comprises u0444u044eu0437u0435u043bu00a0u0436, wing, or other carrier system, propulsion system, the u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0 with u043fu0440u0438u0435u043cu043d u0438u043au043eu043c command radio links, the review system, the transmitter the information signal, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 so that, with a view to u0443u043fu0440u043eu0449u0435u043du0438u00a0 operator work, u0441u043du0438u0436u0435u043du0438u00a0 mas seo, dimensions and cost of aircraftu0443u043bu0443u0447u0448u0435u043du0438u00a0 aerodynamics and u0443u043cu0435u043du044cu0448u0435u043du0438u00a0 errors u0438u0437u043cu0435u0440u0435u043du0438u00a0 coordinates of objects, and also to protect against external influences, u043eu0431u0437u043eu0440u043du0430u00a0 u043au0430u0434u0440u043eu0432u0430u00a0 system is the one or more tv and / or ir cameras and placed inside the u0444u044eu0437u0435u043bu00a0u0436u0430, in the u0444u044eu0437u0435u043bu00a0u0436u0430 carved hole, ensuring personnel review system, review the terrain.;3.u043au0430u0434u0440u043eu0432u0430u00a0 u043eu0431u0437u043eu0440u043du0430u00a0 system remotely manned aircraft u043eu0442u043bu0438u0447u0430u044eu0449u0430u00a0u0441u00a0 so that, with a view to u0443u0432u0435u043bu0438u0447u0435u043du0438u00a0 time u043du0430u0431u043bu044eu0434u0435u043du0438u00a0 object u0443u043bu0443u0447u0448u0435u043du0438u00a0 conditions ville u0440u0430u0441u043fu043eu0437u043du0430u0432u0430u043du0438u00a0 objects and u0441u043du0438u0436u0435u043du0438u00a0 errors u0438u0437u043cu0435u0440u0435u043du0438u00a0 coordinates of objectsthe optical axis of camera review personnel system rigidly fixed in the vertical plane of symmetry of the aircraft, and directed downward and forward under different angles from zero to 90 to the vertical axis of the aircraft, and u043fu043eu043bu00a0 u0437u0440u0435u043du0438u00a0 chambers have different width, and a camera with a u043fu043eu043bu043eu0433u043eu0439 orientation u043eu043fu0442u0438u0447u0435u0441 u043au0438u0445 axes have equal or greater width u043fu043eu043bu00a0 u0437u0440u0435u043du0438u00a0,cells with less than u043fu043eu043bu043eu0433u043eu0439 orientation.;4. u043au0430u0434u0440u043eu0432u0430u00a0 u043eu0431u0437u043eu0440u043du0430u00a0 system remotely manned spacecraft on u043eu0442u043bu0438u0447u0430u044eu0449u0430u00a0u0441u00a0 3, however, that in order to stabilize the u0438u0437u043eu0431u0440u0430u0436u0435u043du0438u00a0 on u043au0440u0435u043du0443 u043eu0431u0437u043eu0440u043du0430u00a0 frame u043eu0432u0430u00a0 system is suspended on the axis parallel to the longitudinal axis of the aircraft and is equipped with the transmission u0434u043bu00a0 rotation around the axis on the top of u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0.;5. u043au0430u0434u0440u043eu0432u0430u00a0 u043eu0431u0437u043eu0440u043du0430u00a0 system remotely manned spacecraft on p.4, u043eu0442u043bu0438u0447u0430u044eu0449u0430u00a0u0441u00a0 however that, in order to protect against external influences, u043eu0431u0437u043eu0440u043du0430u00a0 u043au0430u0434u0440u043eu0432u0430u00a0 system equipped with hard u0441u0432u00a0u0437u0430u043du043du043eu0439 with her when the lid u043au043eu0442u043eu0440u0430u00a0 capacity fourth review system around the axis of suspension at a sufficiently large angle, u043fu0440u0435u0432u043eu0441u0445u043eu0434u00a0u0449u0438u0439 working angles, closes the opening end u0444u044eu0437u0435u043bu00a0u0436u0430 providing personnel u043eu0431u0437u043eu0440u043d oh the review areas.