METHOD AND APPARATUS FOR DETERMINING width of the corridor to safely maneuver the aircraft and METHOD AND SYSTEM SECURITY AUTOMATIC flight of the aircraft at low altitude

摘要

1. method u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 width corridor (cs) safe u043cu0430u043du0435u0432u0440u0438u0440u043eu0432u0430u043du0438u00a0, which u043eu043fu0440u0435u0434u0435u043bu00a0u0435u0442u0441u00a0 on each side of the lateral trajectory (tl) u0434u043bu00a0 trajectory (to) of the summer the implementation of (a).;in which;(a) the many mistakes, u043au0430u0436u0434u0430u00a0 of which u0432u043bu0438u00a0u0435u0442 to automatic flight of the aircraft (a) at low altitude.;(b) u043eu043fu0440u0435u0434u0435u043bu00a0u044eu0442 u0432u0435u0440u043eu00a0u0442u043du043eu0441u0442u044c exit corridor (cs) safe u043cu0430u043du0435u0432u0440u0438u0440u043eu0432u0430u043du0438u00a0, out of which u0434u043eu043fu0443u0441u043au0430u0435u0442u0441u00a0; and;(c) on the basis of u0443u043fu043eu043cu00a0u043du0443u0442u044bu0445 errors and u0443u043fu043eu043cu00a0u043du0443u0442u043eu0439 u0432u0435u0440u043eu00a0u0442u043du043eu0441u0442u0438 exit u043eu043fu0440u0435u0434u0435u043bu00a0u044eu0442 width (d) u0443u043fu043eu043cu00a0u043du0443u0442u043eu0433u043e corridor (cs) safe u043cu0430u043du0435u0432u0440u0438u0440u043eu0432u0430u043du0438u00a0 taking into account at least e, a mathematical u0432u044bu0440u0430u0436u0435u043du0438u00a0 establishing u0432u0437u0430u0438u043cu043eu0441u0432u00a0u0437u044c between at least u0443u043fu043eu043cu00a0u043du0443u0442u044bu043cu0438 errors, u0443u043fu043eu043cu00a0u043du0443u0442u043eu0439 u0432u0435u0440u043eu00a0u0442u043du043eu0441u0442u044cu044e exit and u0443u043fu043eu043cu00a0u043du0443u0442u043eu0439 siri noah (d).;2. the way to 1.;in the stage (a) account for at least some of the following errors.;u043du0430u0432u0438u0433u0430u0446u0438u043eu043du043du0430u00a0 mistake;;error u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0;;the flight path.;3. the way to 1.;which u0443u043fu043eu043cu00a0u043du0443u0442u044bu0435 error value in the form of density u0432u0435u0440u043eu00a0u0442u043du043eu0441u0442u0435u0439.;4. method for p. 3.;which u0443u043fu043eu043cu00a0u043du0443u0442u044bu0435 density u0432u0435u0440u043eu00a0u0442u043du043eu0441u0442u0435u0439 u0443u0434u043eu0432u043bu0435u0442u0432u043eu0440u00a0u044eu0442 to one of the following acts:;the exponential u0440u0430u0441u043fu0440u0435u0434u0435u043bu0435u043du0438u00a0;;the u0440u0430u0441u043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 laplace gauss.;u0440u0430u0441u043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 poisson's law.;the law of polynomial u0440u0430u0441u043fu0440u0435u0434u0435u043bu0435u043du0438u00a0.;5. the way to 1.;which u0443u043fu043eu043cu00a0u043du0443u0442u0430u00a0 u0432u0435u0440u043eu00a0u0442u043du043eu0441u0442u044c exit is equal to 10 - 8 / hdv where hdv denotes an hour flight the aircraft (a).;6. the way to 1.;in the case in which two different errors u0443u043fu043eu043cu00a0u043du0443u0442u043eu0435 u043fu0440u0435u0434u0441u0442u0430u0432u043bu00a0u0435u0442 a mathematical expression;where:;p denotes the u0443u043fu043eu043cu00a0u043du0443u0442u0443u044e u0432u0435u0440u043eu00a0u0442u043du043eu0441u0442u044c withdrawal;;d denotes the half width (d) u0443u043fu043eu043cu00a0u043du0443u0442u043eu0439 corridor (cs) safe u043cu0430u043du0435u0432u0440u0438u0440u043eu0432u0430u043du0438u00a0;;f1 represents the density of u0432u0435u0440u043eu00a0u0442u043du043eu0441u0442u0438, u043eu0442u043du043eu0441u00a0u0449u0443u044eu0441u00a0 to first of u0443u043fu043eu043cu00a0u043du0443u0442u044bu0445 errors; and;ground refers to the density of u0432u0435u0440u043eu00a0u0442u043du043eu0441u0442u0438, u043eu0442u043du043eu0441u00a0u0449u0443u044eu0441u00a0 second mistake.;7. method for p.6.;in which, in the case of three different errors in the individual u043fu043bu043eu0442u043du043eu0441u0442u00a0u043cu0438 fi u0432u0435u0440u043eu00a0u0442u043du043eu0441u0442u0438 also u043fu0440u0438u043cu0435u043du00a0u0435u0442u0441u00a0 u0443u043fu043eu043cu00a0u043du0443u0442u043eu0435 mathematical expression u043fu043eu0437u0432u043eu043bu00a0u044eu0449u0435 (e u0432u044bu0447u0438u0441u043bu00a0u0442u044c p in the form of two density functions f1 and ground u0432u0435u0440u043eu00a0u0442u043du043eu0441u0442u0438, where f1 is the density of u0432u0435u0440u043eu00a0u0442u043du043eu0441u0442u0438 arising from the sum of the two errors with individual u043fu043bu043eu0442u043du043eu0441u0442u00a0u043c and the u0432u0435u0440u043eu00a0u0442u043du043eu0441u0442u0438,and the ground is one of the u0432u0435u0440u043eu00a0u0442u043du043eu0441u0442u0438 third u043eu0441u0442u0430u0432u0448u0435u0439u0441u00a0 mistakes.;8. the way to 1.;which u0443u043fu043eu043cu00a0u043du0443u0442u044bu0435 mistakes u0432u044bu0440u0430u0436u0430u044eu0442u0441u00a0 in form of the law u0440u0430u0441u043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 laplace gauss and the width (d) corridor (cs) safe u043cu0430u043du0435u0432u0440u0438u0440u043eu0432u0430u043du0438u00a0 corresponds with u0443u0434u0432u043eu0435u043du043du043eu043cu0443 u0440u0435u0434u043du0435u043au0432u0430u0434u0440u0430u0442u0438u0447u0435u0441u043au043eu043cu0443 value limits u0443u043fu043eu043cu00a0u043du0443u0442u044bu0445 errors u044du043au0441u0442u0440u0430u043fu043eu043bu0438u0440u043eu0432u0430u043du043du044bu0445 u0434u043bu00a0 trust u0437u043du0430u0447u0435u043du0438u00a0 u0443u043fu043eu043cu00a0u043du0443u0442u043eu0439 u0432u0435u0440u043eu00a0u0442u043du043eu0441u0442u0438 exit.;9. method for u0443u043fu043eu043cu00a0u043du0443u0442u043eu0435 p.8, in which mathematical expression has the form;where:;d denotes the half width (d) u0443u043fu043eu043cu00a0u043du0443u0442u043eu0439 corridor (cs) safe u043cu0430u043du0435u0432u0440u0438u0440u043eu0432u0430u043du0438u00a0;;l (p) u00a0u0432u043bu00a0u0435u0442u0441u00a0 u0440u0430u0437u043bu043eu0436u0435u043du0438u00a0 coefficient, which depends on the u0432u0435u0440u043eu00a0u0442u043du043eu0441u0442u0438 p u043fu043eu00a0u0432u043bu0435u043du0438u00a0 mistakes; and;i mean standard deviation u0440u0430u0441u043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 gaussian errors.;10. the way to 1.;which u0443u043fu043eu043cu00a0u043du0443u0442u043eu0439 width (d) u0434u043eu0431u0430u0432u043bu00a0u044eu0442 admission to wingspan of an aircraft (a).;11. the way to 1.;which include at least one mistake, u043au043eu0442u043eu0440u0430u00a0 due to failure of at least one of the aircraft (a).;12. method u043eu0431u0435u0441u043fu0435u0447u0435u043du0438u00a0 security flight at low altitude aircraft (a), which u043fu0440u043eu0432u043eu0434u0438u0442u0441u00a0 on trajectory (to) the flight of the lateral trajectory (tl ) and the vertical trajectory.;where:;u043eu043fu0440u0435u0434u0435u043bu00a0u044eu0442 width (d) corridor (cs) by way of on the safe u043cu0430u043du0435u0432u0440u0438u0440u043eu0432u0430u043du0438u00a0 1;;u043eu043fu0440u0435u0434u0435u043bu00a0u044eu0442 corridor (cs) safe u043cu0430u043du0435u0432u0440u0438u0440u043eu0432u0430u043du0438u00a0, free from any u043fu0440u0435u043fu00a0u0442u0441u0442u0432u0438u0439, which has u0443u043fu043eu043cu00a0u043du0443u0442u0443u044e width (d) which is limited on each side u0443u043fu043eu043cu00a0u043du0443 the lateral trajectory (tl); and;the aircraft (a) automatically u043fu0440u043eu0432u043eu0434u00a0u0442 on u0443u043fu043eu043cu00a0u043du0443u0442u043eu0439 trajectory (to) flight.;13. the device u0434u043bu00a0 u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 width corridor (cs) safe u043cu0430u043du0435u0432u0440u0438u0440u043eu0432u0430u043du0438u00a0, which u0437u0430u0434u0430u0435u0442u0441u00a0 on each side of the lateral trajectory (tl) u0434u043bu00a0 trajectory (to) flight l u0435u0442u0430u0442u0435u043bu044cu043du043eu0433u043e apparatus (a).;in this u0443u043fu043eu043cu00a0u043du0443u0442u043eu0435 device contains:;a means (3), u043fu0440u0435u0434u043eu0441u0442u0430u0432u043bu00a0u044eu0449u0435u0435 opportunity to many mistakes, u043au0430u0436u0434u0430u00a0 of which u0432u043bu0438u00a0u0435u0442 to automatic flight at low altitude aircraft (a);;a means (4) u0434u043bu00a0 u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 u0432u0435u0440u043eu00a0u0442u043du043eu0441u0442u0438 exit corridor (cs) safe u043cu0430u043du0435u0432u0440u0438u0440u043eu0432u0430u043du0438u00a0, out of which u0434u043eu043fu0443u0441u043au0430u0435u0442u0441u00a0; and;a means (5) u0434u043bu00a0 u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 width (d) u0443u043fu043eu043cu00a0u043du0443u0442u043eu0433u043e corridor (cs) based on the safe u043cu0430u043du0435u0432u0440u0438u0440u043eu0432u0430u043du0438u00a0 u0443u043fu043eu043cu00a0u043du0443u0442u044bu0445 errors and u0443u043fu043eu043cu00a0u043du0443u0442u043eu0439 u0432u0435u0440u043eu00a0u0442u043du043eu0441u0442u0438 way taking into account. at least one mathematical u0432u044bu0440u0430u0436u0435u043du0438u00a0 establishing u0432u0437u0430u0438u043cu043eu0441u0432u00a0u0437u044c between at least u0443u043fu043eu043cu00a0u043du0443u0442u044bu043cu0438 errors, u0443u043fu043eu043cu00a0u043du0443u0442u043eu0439 u0432u0435u0440u043eu00a0u0442u043du043eu0441u0442u044cu044e exit and u043fu043eu043cu00a0u043du0443u0442u043eu0439 width (d).;14. the system u0434u043bu00a0 u043eu0431u0435u0441u043fu0435u0447u0435u043du0438u00a0 security flight at low altitude aircraft (a), with u0443u043fu043eu043cu00a0u043du0443u0442u0430u00a0 system (9) contains:;the first tool (10) u0434u043bu00a0 u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 trajectory (to) the flight of the lateral trajectory (tl) and vertical trajectory; and;a means (11) u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0 u0434u043bu00a0 automatic u043fu0440u043eu0432u0435u0434u0435u043du0438u00a0 aircraft (a) u0443u043fu043eu043cu00a0u043du0443u0442u043eu0439 trajectory (to) flight, containing also the navigation tool;in this u0443u043fu043eu043cu00a0u043du0443u0442u0430u00a0 system additionally contains:;the device (1), in particular, p.13 u0434u043bu00a0 u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 width (d) of the safe u043cu0430u043du0435u0432u0440u0438u0440u043eu0432u0430u043du0438u00a0 (cs); and;the second means (17) u0434u043bu00a0 u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 corridor (cs) safe u043cu0430u043du0435u0432u0440u0438u0440u043eu0432u0430u043du0438u00a0, free from any u043fu0440u0435u043fu00a0u0442u0441u0442u0432u0438u0439, which has u0443u043fu043eu043cu00a0u043du0443u0442u0443u044e width (d), a u0443u043fu043eu043c u00a0u043du0443u0442u044bu043c device (1), and which is limited on each side u0443u043fu043eu043cu00a0u043du0443u0442u043eu0439 horizontal trajectory (tl).;15. aircraft containing the device (1) providing the way to 1.;16. aircraft containing system (9) provides the way on p.12.;17. aircraft containing the device (1), p.13.;18. aircraft containing system (9), p.14.