METHOD FOR DETERMINING maximum power output of solar cells spacecraft and SYSTEM FOR CARRYING OUT

摘要

1.method u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 maximum power output of solar panels of a spacecraft, consisting of a solar panels in the working position, with the u043eu043eu0442u0432u0435u0442u0441u0442u0432u0443u044eu0449u0435u0435 combining u043du043eu0440u043cu0430u043bu0438 to illuminated working surface with the direction of the sun, u0437u043du0430u0447u0435u043du0438u00a0 measurement current from solar cellsmeasurement of u043du0430u043fu0440u00a0u0436u0435u043du0438u00a0 and determination of the maximum power output of solar panels of a spacecraft as the product of the measured values u043du0430u043fu0440u00a0u0436u0435u043du0438u00a0 and look from the solar cells, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 orderfurther u0438u0437u043cu0435u0440u00a0u044eu0442 orbital altitude of the spacecraft and u043eu043fu0440u0435u0434u0435u043bu00a0u044eu0442 on her u0437u043du0430u0447u0435u043du0438u00a0 of u043fu043eu043bu0443u0440u0430u0441u0442u0432u043eu0440u0430 visible from the spacecraft earth (disk Qz) and the u0432u043eu0437u0432u044bu0448u0435u043du0438u00a0 upper atmosphere over the visible horizon with spacecraft earth (), u043eu043fu0440u0435u0434u0435u043bu00a0u044eu0442 importance of u043fu043eu043bu0443u0440u0430u0441u0442u0432u043eu0440u0430 visible from space technical apparatus of disk sun (qs)u0438u0437u043cu0435u0440u00a0u044eu0442 u0443u0433u043bu043eu0432u0443u044e speed orbital u0434u0432u0438u0436u0435u043du0438u00a0 spacecraft (), u0438u0437u043cu0435u0440u00a0u044eu0442 angle between the direction of the sun and the plane of the orbit of the spacecraft () on the u0432u0438u0442u043au0430u0445, at which the importance of u0438u0437u043cu0435u0440u00a0u0435u043cu043eu0433u043e angle less than or equal to the value, u043eu043fu0440u0435u0434u0435u043bu00a0u0435u043cu043eu043cu0443 formula;= arccos {cosQz / cos (t / 2)},;where t is the minimum length of the shadow of u0442u0440u0435u0431u0443u0435u043cu0430u00a0 u0434u043eu043fu0443u0441u0442u0438u043cu0430u00a0 orbit orbit;u0438u0437u043cu0435u0440u00a0u044eu0442 corner u0432u043eu0437u0432u044bu0448u0435u043du0438u00a0 u043du0430u043fu0440u0430u0432u043bu0435u043du0438u00a0 in the sun above the horizon visible from the spacecraft ground (g), and the maximum output power of solar batteries in them the minimum temperature u043eu043fu0440u0435u0434u0435u043bu00a0u044eu0442 as the product of the values of the u043du0430u043fu0440u00a0u0436u0435u043du0438u00a0 and current from the solar cells, measured at the time of u043au0430u0441u0430u043du0438u00a0 visible from space. the upper boundary of the earth's atmosphere and with the sun at sunriseu043eu043fu0440u0435u0434u0435u043bu00a0u0435u043cu044bu0439 of u0443u0441u043bu043eu0432u0438u00a0 equality u0437u043du0430u0447u0435u043du0438u00a0 u0438u0437u043cu0435u0440u00a0u0435u043cu043eu0433u043e angle g amount values of qs in the growing u0437u043du0430u0447u0435u043du0438u00a0 angle g, and the maximum output power u0441u043eu043bu043du0435u0447u043du044b the cells at the maximum working temperature u0443u0441u0442u0430u043du043eu0432u0438u0432u0448u0435u0439u0441u00a0 u043eu043fu0440u0435u0434u0435u043bu00a0u044eu0442 as the product of the values of the u043du0430u043fu0440u00a0u0436u0435u043du0438u00a0 and current from the solar cellsmeasured at the time of u043au0430u0441u0430u043du0438u00a0 visible from the spacecraft or the upper boundary of the sun the earth's atmosphere at sundown, u043eu043fu0440u0435u0434u0435u043bu00a0u0435u043cu044bu0439 of u0443u0441u043bu043eu0432u0438u00a0 equality kn u0430u0447u0435u043du0438u00a0 u0438u0437u043cu0435u0440u00a0u0435u043cu043eu0433u043e angle g amount values of qs in the u0443u0431u044bu0432u0430u043du0438u0438 u0437u043du0430u0447u0435u043du0438u00a0 angle g.;2.the system u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 maximum power output of solar panels of a spacecraft, u0432u043au043bu044eu0447u0430u044eu0449u0430u00a0 solar battery with a set on her u0444u043eu0442u043eu044du043bu0435 u043au0442u0440u0438u0447u0435u0441u043au0438u0445 batteries, the device of solar cell u0443u0441u0438u043bu0438u0442u0435u043bu044cu043du043e - converts the device, block u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0 orientation of solar cells in a direction n and the sun block u0440u0435u0433u0443u043bu00a0u0442u043eu0440u043eu0432 current sensor, current, the u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 powerthe u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0 system u044du043bu0435u043au0442u0440u043eu0441u043du0430u0431u0436u0435u043du0438u00a0 and tire u044du043bu0435u043au0442u0440u043eu0441u043du0430u0431u0436u0435u043du0438u00a0, with the exit block is connected to the entrance of the block u0440u0435u0433u0443u043bu00a0u0442u043eu0440u043eu0432 pv power tips of which is connected with the splint u044du043bu0435u043au0442u0440u043eu0441u043du0430u0431u0436u0435u043du0438u00a0 to which are connected a current and block u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 powerand the output unit is connected to the first u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0 system u044du043bu0435u043au0442u0440u043eu0441u043du0430u0431u0436u0435u043du0438u00a0 entrance block u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0 orientation of solar cells in the direction of the sun, up to wow is connected with the entrance u0443u0441u0438u043bu0438u0442u0435u043bu044cu043du043e - transformational device which is connected with the entrance exit device of solar cellthe exit of which is connected with the second entrance block u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0 orientation of solar cells in the direction of the sun, solar lamps, and device u0435u0445u0430u043du0438u0447u0435u0441u043au0438 electrically connected with the solar battery u043eu0442u043bu0438u0447u0430u044eu0449u0430u00a0u0441u00a0, added the u0438u0437u043cu0435u0440u0435u043du0438u00a0 angle between the direction of the sun and the plane of the orbit well u0438u0447u0435u0441u043au043eu0433u043e apparatusthe u0438u0437u043cu0435u0440u0435u043du0438u00a0 angle u0432u043eu0437u0432u044bu0448u0435u043du0438u00a0 u043du0430u043fu0440u0430u0432u043bu0435u043du0438u00a0 in the sun above the horizon the earth visible from the spacecraft angular velocity, the u0438u0437u043cu0435u0440u0435u043du0438u00a0 orbital move u00a0 spacecraft, block u0438u0437u043cu0435u0440u0435u043du0438u00a0 high orbit spacecraft, block u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 angle u0432u043eu0437u0432u044bu0448u0435u043du0438u00a0 upper atmosphere earth visible from the well the apparatus u0438u0447u0435u0441u043au043eu0433u043e horizon of earththe u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 angle u043fu043eu043bu0443u0440u0430u0441u0442u0432u043eu0440u0430 visible with the spacecraft orbit the sun disk, the u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 u0432u044bu043fu043eu043bu043du0435u043du0438u00a0 operation u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 maximum output solar powered, block u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 points u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 maximum power output of solar cells, the u0444u043eu0440u043cu0438u0440u043eu0432u0430u043du0438u00a0 identification u043fu0430u0440u0430u043cu0435 u0442u0440u043eu0432 temperature of solar batteries and keythe second input unit u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 power is connected with the access key information and u0443u043fu0440u0430u0432u043bu00a0u044eu0449u0438u0439 entrances which are connected respectively with the outputs of sensor a current and block u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 points u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 maximum power output of solar cells.the first to fourth entrances which are connected to the outputs, respectively, of the u0438u0437u043cu0435u0440u0435u043du0438u00a0 u0432u043eu0437u0432u044bu0448u0435u043du0438u00a0 u043du0430u043fu0440u0430u0432u043bu0435u043du0438u00a0 sun over the visible in the outer u0430u043fu043fu0430u0440 ata horizon land block u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 angle u043fu043eu043bu0443u0440u0430u0441u0442u0432u043eu0440u0430 visible with spacecraft drive sunthe upper boundary of u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 u0432u043eu0437u0432u044bu0448u0435u043du0438u00a0 earth's atmosphere over the visible from the spacecraft orbit the earth and the horizon u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 u0432u044bu043fu043eu043bu043du0435u043du0438u00a0 operating unit the radio u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 maximum power output of solar panels, first, second and third inlet which are connected with the outputs of u0438u0437u043cu0435u0440u0435u043du0438u00a0 have respectively u0433u043bu0430 between the direction of the sun and the plane of the orbit of the spacecraft.block u0438u0437u043cu0435u0440u0435u043du0438u00a0 angular velocity u0434u0432u0438u0436u0435u043du0438u00a0 orbital spacecraft and block u0438u0437u043cu0435u0440u0435u043du0438u00a0 high orbit spacecraft, the exit that is so with the entrance of the upper boundary of the earth's atmosphere u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 u0432u043eu0437u0432u044bu0448u0435u043du0438u00a0 over visible from the spacecraft, the horizon of the earth.and the outlet of the u0438u0437u043cu0435u0440u0435u043du0438u00a0 u0432u043eu0437u0432u044bu0448u0435u043du0438u00a0 u043du0430u043fu0440u0430u0432u043bu0435u043du0438u00a0 in the sun above the horizon visible from the spacecraft earth also is connected with the entrance block u0444u043eu0440u043cu0438u0440u043eu0432u0430u043du0438u00a0 id u0435u043du0442u0438u0444u0438u043au0430u0446u0438u043eu043du043du044bu0445 temperature parameters of solar cells, the exit of which is connected with the third entrance block u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 power.