CAREER the aircraft for operations in outer space on the target spacecraft SERVICE SYSTEM AND METHOD OF ADMINISTRATION OFFICIAL AIRCRAFT

摘要

1. a machine (6) u0434u043bu00a0 u043fu0440u043eu0432u0435u0434u0435u043du0438u00a0 operations in outer space at the selected target outer aircraft (2) containing the 60) u0441u0432u00a0u0437u0438 which is designed with the possibility of u043au043eu043du0444u0438u0433u0443u0440u0438u0440u043eu0432u0430u043du0438u00a0 characteristics of transfer and / or receiving u0434u043bu00a0 u0443u0434u043eu0432u043bu0435u0442u0432u043eu0440u0435u043du0438u00a0 given parameters of the receiver and / or control panels u0442u0447u0438u043au0430 selected target spacecraft (2).;2. a machine for u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 1, so that the module (60) u0441u0432u00a0u0437u0438 contains a transmitter (66).;3. a machine for u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 1, so that the module (60) u0441u0432u00a0u0437u0438 contains u043au043eu043du0444u0438u0433u0443u0440u0438u0440u0443u0435u043cu044bu0439 receiver (80).;4. a machine for u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 3, so that the receiver (80) is made adjustable working frequency u0434u043bu00a0 u0441u0432u00a0u0437u0438 with u0442u0435u043bu0435u043cu0435u0442u0440u0438u0447u0435u0441u043au0438u043c channel is selected left the spacecraft (2).;5. service aircraft on 1, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 that additionally contains a module (68) u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0 designed u0434u043bu00a0 u0437u0430u0434u0430u043du0438u00a0 power output u0443u0441u0442u0430u0432u043au0438 mo u0434u0443u043bu00a0 (60) u0441u0432u00a0u0437u0438.;6. business aircraft under clause 5, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0, module (68) u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0 connected with front first sensor u043fu043eu043bu043eu0436u0435u043du0438u00a0, which produces a set of data, ha the current situation of u0440u0430u043au0442u0435u0440u0438u0437u0443u044eu0449u0438u0439 aircraft (6).;7. a machine for p.6, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0, module (68) connected to its gate to the second sensor u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0 u043fu043eu043bu043eu0436u0435u043du0438u00a0 which delivers the data set x the current situation of u0430u0440u0430u043au0442u0435u0440u0438u0437u0443u044eu0449u0438u0439 target spacecraft (2).;8. service aircraft on any of the u043fu043f.5 u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 7, so that the module (68) u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0 is connected with the entrance sensor orientation, which produces a set of dunn s of the current orientation of the target spacecraft (2) for an aircraft (6).;9. service aircraft on any of the u043fu043f.1 - 7, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 that additionally contains a system (24) docking, u043au043eu0442u043eu0440u0430u00a0 contains a hollow first axis (40) inside to the torah is the possibility of u043fu0435u0440u0435u043cu0435u0449u0435u043du0438u00a0 u0432u0442u043eu0440u0430u00a0 axis (42), which is activated u0441u0442u0440u0435u043bu044cu0447u0430u0442u044bu0439 sharp.;10. service aircraft on p.8, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 that additionally contains a system (24) docking, u043au043eu0442u043eu0440u0430u00a0 contains a hollow first axis (40), in which u0440u0430u0441u043fu043eu043b u043eu0436u0435u043du0430 with opportunity u043fu0435u0440u0435u043cu0435u0449u0435u043du0438u00a0 u0432u0442u043eu0440u0430u00a0 axis (42), which is activated u0441u0442u0440u0435u043bu044cu0447u0430u0442u044bu0439 sharp.;11. service aircraft on any of the u043fu043f.1 - 7, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 that additionally contains an identification of the target space aircraft u0434u043bu00a0 ams arata (2).;12. the system (1) u043eu0431u0441u043bu0443u0436u0438u0432u0430u043du0438u00a0 u0434u043bu00a0 u043fu0440u043eu0432u0435u0434u0435u043du0438u00a0 operations in outer space at the selected target outer aircraft (2), u0441u043eu0434u0435u0440u0436u0430u0449u0430u00a0 service u043bu0435u0442u0430u0442u0435 u043bu044cu043du044bu0439 apparatus (6) for any of the u043fu043f.1 - 11 and further u0441u043eu0434u0435u0440u0436u0430u0449u0430u00a0 ground module (12) u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0 u0434u043bu00a0 of working teams to service aircraft (6).;13. the system u043eu0431u0441u043bu0443u0436u0438u0432u0430u043du0438u00a0 on p.12, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 what ground module (12) configured for receiving data from u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0 official aircraft (6), with the task to u0441u043cu0438u0447u0435u0441u043au0438u0439 aircraft (2) serves as the u0440u0435u0442u0440u0430u043du0441u043bu00a0u0446u0438u043eu043du043du043eu0439 station u0434u043bu00a0 signals produced by these aircraft from the service (6).;14. the system u043eu0431u0441u043bu0443u0436u0438u0432u0430u043du0438u00a0 on any of u043eu0442u043bu0438u0447u0430u044eu0449u0430u00a0u0441u00a0 p.12 or 13, so that additionally contains located on orbit working base (4) u0434u043bu00a0 official aircraft appa rata (6).;15. the system u043eu0431u0441u043bu0443u0436u0438u0432u0430u043du0438u00a0 on p.14, u043eu0442u043bu0438u0447u0430u044eu0449u0430u00a0u0441u00a0 that additionally contains u0440u0435u0442u0440u0430u043du0441u043bu00a0u0446u0438u043eu043du043du044bu0439 module u0434u043bu00a0 transmitted signals and forwarding service aircraft u043fu043fu0430u0440u0430u0442u0443 (6).;16. the system u043eu0431u0441u043bu0443u0436u0438u0432u0430u043du0438u00a0 on any of u043eu0442u043bu0438u0447u0430u044eu0449u0430u00a0u0441u00a0 p.12 or 15, so that additionally contains the module of engines is the possibility of u0437u0430u043au0440u0435u043fu043bu0435u043du0438u00a0 a or b u043eu043bu0435u0435 elements working agent, an aircraft, or a target spacecraft.;17. method u043eu0431u0441u043bu0443u0436u0438u0432u0430u043du0438u00a0 target spacecraft (2) in outer space, including the following operations: use of company aircraft apparatus (6) for any of the ap.1 - 11 u0434u043bu00a0 u043fu0440u043eu0432u0435u0434u0435u043du0438u00a0 the operations in outer space target outer aircraft (2) use the u0442u0435u043bu0435u043cu0435u0442u0440u0438u0447u0435u0441u043au0438u0439 channel between land m u043eu0434u0443u043bu0435u043c (12) u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0 and target space aircraft (2) u0434u043bu00a0 u0440u0435u0442u0440u0430u043du0441u043bu00a0u0446u0438u0438 command signals in a machine (6).;18. method u043eu0431u0441u043bu0443u0436u0438u0432u0430u043du0438u00a0 target spacecraft (2) in outer space, including the following operations: use of company aircraft apparatus (6) for any of the ap.1 - 11 u0434u043bu00a0 u043fu0440u043eu0432u0435u0434u0435u043du0438u00a0 the operations in outer space target outer aircraft (2) use of remote u0443u043fu0440u0430u0432u043bu0435u043du0438 channel commands u00a0 between ground module (12) u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0 and target space aircraft (2) u0434u043bu00a0 u0440u0435u0442u0440u0430u043du0441u043bu00a0u0446u0438u0438 command signals in a machine (6).