METHOD OF POWER CONSUMPTION orbital constellation spacecraft with electric propulsion

摘要

method u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0 u044du043bu0435u043au0442u0440u043eu043fu043eu0442u0440u0435u0431u043bu0435u043du0438u0435u043c orbital constellation spacecraft with u044du043bu0435u043au0442u0440u043eu0440u0435u0430u043au0442u0438u0432u043du044bu043cu0438 u0434u0432u0438u0433u0430u0442u0435u043bu00a0u043cu0438 including dimensioning've u043eu043fu043eu0442u0440u0435u0431u043bu0435u043du0438u00a0 each of (i - x on-board user payload (ni), where i = 1, 2, 3,..., i is the total number of consumers by j - x spacecraft, where j = 1, 2, 3 ...is the total number of spacecraft, u0432u0445u043eu0434u00a0u0449u0438u0445 in orbital space group determination kj - x intervals u0434u043bu00a0 u043fu0440u043eu0432u0435u0434u0435u043du0438u00a0 dynamic regimes using of the u044du043bu0435u043au0442u0440u043eu0440u0435u0430u043au0442u0438u0432u043du044bu0445 engines, u0434u043bu00a0 each j th spacecraft, where kj = (1, 2, 3,...K) j, dimensioning u044du043bu0435u043au0442u0440u043eu043fu043eu0442u0440u0435u0431u043bu0435u043du0438u00a0 Ndj each dj - x u044du043bu0435u043au0442u0440u043eu0440u0435u0430u043au0442u0438u0432 for engines, where dj = (1, 2, 3,...d) j is the number of these engines are installed on each j, spacecraft, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0, prior to the simultaneous u043fu0440u043eu0432u0435u0434u0435u043du0438u00a0 mi space appa u0440u0430u0442u0430u043cu0438 - x dynamic regimes of Kj, u043eu043fu0440u0435u0434u0435u043bu00a0u044eu0442 electric power u043fu043eu0442u0440u0435u0431u043bu00a0u0435u043cu0443u044e u044du043bu0435u043au0442u0440u043eu0440u0435u043au0442u0438u0432u043du044bu043cu0438 u0434u0432u0438u0433u0430u0442u0435u043bu00a0u043cu0438 at each meeting, spacecraft;where is the number of u044du043bu0435u043au0442u0440u043eu0440u0435u0430u043au0442u0438u0432u043du044bu0445 engines owned by the dj, involved in the dynamic regime of each meeting, spacecraft, u043eu043fu0440u0435u0434u0435u043bu00a0u044eu0442've u0438u0447u0435u0441u043au0443u044e power u043fu043eu0442u0440u0435u0431u043bu00a0u0435u043cu0443u044e payload for each of the spacecraft, the dynamic regimes of interval;where is the number of units of useful load of i - m serial u043fu043eu0442u0440u0435u0431u0438u0442u0435u043bu00a0u043c payload included on board each of the spacecraft in a the - x dynamic regimes, u043fu0440u043eu0432u0435u0440u00a0u044eu0442 implementation conditions;where is the power of electricity produced on board each of the spacecraft, the dynamic regimes at any interval.;- the power of electricity, u043fu043eu0442u0440u0435u0431u043bu00a0u0435u043cu043eu0439 official systems of each of the spacecraft, the dynamic regimes - x intervals;and if u0443u0441u043bu043eu0432u0438u00a0 (1) u0432u044bu043fu043eu043bu043du00a0u044eu0442u0441u00a0, u043eu0441u0443u0449u0435u0441u0442u0432u043bu00a0u044eu0442 the - x dynamic regimes, and if any of u0434u043bu00a0 spacecraft condition (1) u0432u044bu043fu043eu043bu043du00a0u0435u0442u0441u00a0, u043eu043fu0440u0435u0434u0435u043bu00a0 s u0434u043bu00a0 him th interval belonging to the meeting, u0438u043du0442u0435u0440u0432u0430u043bu0430u043c time u0434u043bu00a0 that condition (1) u0432u044bu043fu043eu043bu043du00a0u0435u0442u0441u00a0 and u043eu0441u0443u0449u0435u0441u0442u0432u043bu00a0u044eu0442 the dynamic regime of the integration u0440u0432u0430u043bu0435,if condition (1) u0432u044bu043fu043eu043bu043du00a0u0435u0442u0441u00a0 u0434u043bu00a0 all interval u043fu0440u043eu0438u0437u0432u043eu0434u00a0u0442 definition u0432u0445u043eu0434u00a0u0449u0438u0445 in orbital constellation - x spacecraft - the second string, u0440u0430u0432u043du043eu0437u043d u0430u0447u043du044bu0445 functions the payloadu043fu0440u043eu0432u0435u0440u00a0u044eu0442 u0434u043bu00a0 each of x spacecraft - alternates the conditions u043eu0431u0435u0441u043fu0435u0447u0435u043du0438u00a0 u044du043bu0435u043au0442u0440u043eu043fu043eu0442u0440u0435u0431u043bu0435u043du0438u00a0 while switching them in the consumer field the heat load with the - x spacecraft;where is the power of electricity produced on board each of the spacecraft's understudy in the meeting, the interval u043fu0440u043eu0432u0435u0434u0435u043du0438u00a0 dynamic regime.;- the power of electricity, u043fu043eu0442u0440u0435u0431u043bu00a0u0435u043cu043eu0439 u043fu0435u0440u0435u043au043bu044eu0447u0435u043du043du043eu0439 part of consumers of spacecraft payload with the th spacecraft - the understudy to the meeting, vin u0435u0440u0432u0430u043bu0435 u043fu0440u043eu0432u0435u0434u0435u043du0438u00a0 dynamic regime.;- the power of electricity, u043fu043eu0442u0440u0435u0431u043bu00a0u0435u043cu043eu0439 payload of spacecraft - the understudy to - m span u043fu0440u043eu0432u0435u0434u0435u043du0438u00a0 dynamic regime.;- the power of electricity, u043fu043eu0442u0440u0435u0431u043bu00a0u0435u043cu043eu0439 official systems of each of the spacecraft's understudy, u0432u043au043bu044eu0447u0430u00a0 electroactive engines the dinami as regimes, interval, and the th spacecraft - u0434u0443u0431u043bu0435u0440u0430u043c, u0434u043bu00a0 which u0443u0441u043bu043eu0432u0438u00a0 (2) u0432u044bu043fu043eu043bu043du00a0u044eu0442u0441u00a0, u043fu0440u043eu0438u0437u0432u043eu0434u00a0u0442 consistent u043fu043eu0434u043au043bu044eu0447u0435u043du0438u00a0 those u043fu043eu0442u0440u0435u0431u0438u0442 oil payload with - x spacecraftwith the necessary supplies of electricity - x spacecraft - the second string to u0432u044bu043fu043eu043bu043du0435u043du0438u00a0 conditions (1) - x spacecraft and u043eu0441u0443u0449u0435u0441u0442u0432u043bu00a0u044eu0442 about u0432u0435u0434u0435u043du0438u00a0 dynamic regimes - mi spacecraft on x in the interval, and the conditions (2) and, while not meeting the conditions (1).u043fu0440u043eu0438u0437u0432u043eu0434u00a0u0442 consistent shutdown unsecured electricity - x spacecraft - the second string (i - x side, consumers payload set during the - x spacecraft, to u0432u044bu043fu043eu043bu043du0435u043du0438u00a0 u0443u0441u043bu043eu0432u0438u00a0 (1) and u043eu0441u0443u0449u0435u0441u0442u0432u043bu00a0u044eu0442 the dynamic regimes of the time interval u0434u043bu00a0 - x space u0430u043fu043fu0430u0440 no blame on you if you.further follow-up u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0 u044du043bu0435u043au0442u0440u043eu043fu043eu0442u0440u0435u0431u043bu0435u043du0438u0435u043c orbital groups u043fu0440u043eu0438u0437u0432u043eu0434u00a0u0442 consistently in the above manner, u0434u043bu00a0 spacecraft with a p u043eu0437u0434u043du0438u043c start time u043fu0440u043eu0432u0435u0434u0435u043du0438u00a0 dynamic regimes, u0438u0441u043fu043eu043bu044cu0437u0443u00a0 with - e spacecraft as understudies for the subsequent dynamic r u0435u0436u0438u043cu043eu0432 other spacecraft.