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, further u0438u0437u043cu0435u0440u00a0u044eu0442 angle between the direction of the sun and the plane of the orbit of the spacecraft, u0432u0438u0442u043au0430u0445, to u043eu0442u043eu0440u044bu0445 value angleequal 180 minus the amount of the u043fu043eu043bu0443u0440u0430u0441u0442u0432u043eu0440u0430 visible from the spacecraft and the earth u043fu043eu043bu0443u0440u0430u0441u0442u0432u043eu0440u0430 disk zone of the working surface u0441u043eu043bu043du0435u0447u043du044b x battery exceeds the measured above the angle u0438u0437u043cu0435u0440u00a0u044eu0442 corner u0432u043eu0437u0432u044bu0448u0435u043du0438u00a0 u043du0430u043fu0440u0430u0432u043bu0435u043du0438u00a0 in the sun above the horizon is visible from the spacecraft lands, and the maximum you u0445u043eu0434u043du0443u044e power bilateral solar panels and solar cellshaving a positive output power of their back surfaces u043eu043fu0440u0435u0434u0435u043bu00a0u044eu0442 as the product of the values of the u043du0430u043fu0440u00a0u0436u0435u043du0438u00a0 and current from the solar cells, measured in time s, in which the radiation is reflected from the earth to the solar panels with their end sides.u043eu043fu0440u0435u0434u0435u043bu00a0u0435u043cu044bu0435 u0443u0441u043bu043eu0432u0438u00a0 equality of values of the u0432u043eu0437u0432u044bu0448u0435u043du0438u00a0 u043du0430u043fu0440u0430u0432u043bu0435u043du0438u00a0 sun above the horizon visible from earth and the spacecraft u043fu043eu043bu0443u0440u0430u0441u0442u0432u043eu0440u0430 zone h u0443u0432u0441u0442u0432u0438u0442u0435u043bu044cu043du043eu0441u0442u0438 working surface of solar panels, and the maximum output power of solar cell as a unilateral u043eu043fu0440u0435u0434u0435u043bu00a0u044eu0442 kn u0430u0447u0435u043du0438u0439 u043du0430u043fu0440u00a0u0436u0435u043du0438u00a0 and current from the solar cells, measured in points.in which radiation reflected from the earth is on solar panels with their face or the back of the u043eu043fu0440u0435u0434u0435u043bu00a0u0435u043cu044bu0435 of u0443u0441u043bu043eu0432u0438u00a0 equality or u043fu0440u0435u0432u044bu0448u0435u043du0438u00a0 the value of the u0432u043eu0437u0432u044bu0448u0435u043du0438u00a0 u043du0430u043fu0440u0430u0432u043bu0435u043du0438u00a0 in the sun above the horizon the earth visible from the spacecraft u043fu043eu043bu0443u0440u0430u0441u0442u0432u043eu0440u0430 zone working u043fu043eu0432u0435u0440u0445u043du043eu0441 sensitivity t of solar cells.;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 cycle of operation u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 u0432u044bu043fu043eu043bu043du0435u043du0438u00a0 u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 maximum power output of solar cells, the u0438u0437u043cu0435u0440u0435u043du0438u00a0 angle u0432u043eu0437u0432u044bu0448u0435u043du0438u00a0 u043du0430u043fu0440u0430u0432u043bu0435u043du0438u00a0 sun n the fire visible from the spacecraft earth horizon, block u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 moment u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 maximum power output of solar cells and the key, and u0432u0442u043eu0440 oh the entrance block u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 power is connected with the exit keyinformation and u0443u043fu0440u0430u0432u043bu00a0u044eu0449u0438u0439 entrances which are connected with the current sensor and outputs, respectively, of the u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 maximum output capacities of the solar cell, which is connected with an entrance of the u0438u0437u043cu0435u0440u0435u043du0438u00a0 u0432u043eu0437u0432u044bu0448u0435u043du0438u00a0 u043du0430u043fu0440u0430u0432u043bu0435u043du0438u00a0 in the sun above the horizon and visible from the spacecraft u0435u043cu043bu0438,the entrance which is connected with the exit of the cycle of operation u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 u0432u044bu043fu043eu043bu043du0435u043du0438u00a0 u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 maximum power output of solar cells, the entrance of which u0441u043eu0435u0434u0438u043d yong an angle between the direction of the block u0438u0437u043cu0435u0440u0435u043du0438u00a0 sun and the plane of the orbit of the spacecraft.