METHOD AND DEVICE FOR AIRCRAFT collision avoidance with obstacles in adverse weather conditions

摘要

1.method u043fu0440u0435u0434u0443u043fu0440u0435u0436u0434u0435u043du0438u00a0 u0441u0442u043eu043bu043au043du043eu0432u0435u043du0438u00a0 aircraft with u043fu0440u0435u043fu00a0u0442u0441u0442u0432u0438u00a0u043cu0438 in complex u043cu0435u0442u0435u043eu0443u0441u043bu043eu0432u0438u00a0u0445, u0437u0430u043au043bu044eu0447u0430u044eu0449u0438u0439u0441u00a0 is u0437u043du0430u0447u0435u043du0438u00a0 u0440u0430u0441u0441u0442u043eu00a0u043du0438u00a0 ams aircraft arata to u043fu0440u0435u043fu00a0u0442u0441u0442u0432u0438u00a0 u043eu043fu0440u0435u0434u0435u043bu00a0u044eu0442 using on-board radar and on the basis of data obtained by the information processing system of the satellite u043du0430u0432u0438u0433u0430 from the angles of system u0438u0437u043cu0435u0440u0435u043du0438u00a0 list, pitch,the course and a travel speed and the on-board devices u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 aeronautical data, so that the formed u0437u043du0430u0447u0435u043du0438u00a0 u0440u0430u0441u0441u0442u043eu00a0u043du0438u00a0 aircraft to p u0440u0435u043fu00a0u0442u0441u0442u0432u0438u00a0 u043du0430u043fu0440u0430u0432u043bu00a0u044eu0442 simultaneously in the computing system, and by u0441u0440u0430u0432u043du0435u043du0438u00a0 them to choose, which goes beyond the limit.and on its basis the shape signal and transmit the alarm u043fu0440u0435u0434u0443u043fu0440u0435u0436u0434u0435u043du0438u00a0 crew of the danger.;2.the device u043fu0440u0435u0434u0443u043fu0440u0435u0436u0434u0435u043du0438u00a0 u0441u0442u043eu043bu043au043du043eu0432u0435u043du0438u00a0 aircraft with u043fu0440u0435u043fu00a0u0442u0441u0442u0432u0438u00a0u043cu0438 in complex u043cu0435u0442u0435u043eu0443u0441u043bu043eu0432u0438u00a0u0445 containing on-board radar satellite system at u0432u0438u0433u0430u0446u0438u0438, on-board aeronautical data loader system u0438u0437u043cu0435u0440u0435u043du0438u00a0 corners of list, pitch and ground speed of flight, for example u0438u043du0435u0440u0446u0438u0430u043bu044cu043du0443u044e system perf u0438u0447u0430u044eu0449u0435u0435u0441u00a0 in that it is u0432u044bu0447u0438u0441u043bu0438u0442u0435u043bu044cu043du0430u00a0 systemwhich introduced a software module at the same time, acquires information on the whereabouts of la from the satellite navigation system, the system u0438u0437u043cu0435u0440u0435u043du0438u00a0 corners of list, etc. u0430u043du0433u0430u0436u0430 and course, and a travel speed, and the on-board devices and aeronautical data signal u0440u0430u0441u0441u0442u043eu00a0u043du0438u00a0 before arriving u0432u043cu0435u0441u0442 u043fu0440u0435u043fu00a0u0442u0441u0442u0432u0438u00a0 intestine e with the information from the on-board radar to the software u043cu043eu0434u0443u043bu00a0,united with the alarm system u043fu0440u0435u0434u0443u043fu0440u0435u0436u0434u0435u043du0438u00a0 crew about the danger u0441u0440u0430u0431u0430u0442u044bu0432u0430u044eu0449u0435u0439 from the signal received by u0441u0440u0430u0432u043du0435u043du0438u00a0 values u0440u0430u0441u0441u0442u043eu00a0u043du0438u0439 to u043fu0440u0435u043fu00a0u0442u0441u0442 u0432u0438u00a0 and select the most dangerous one.