首页> 外国专利> System for determining maximum power output of solar cells SPACECRAFT

System for determining maximum power output of solar cells SPACECRAFT

机译:确定太阳能电池最大功率输出的系统SPACECRAFT

摘要

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 apparatus, block u0438u0437u043cu0435u0440u0435u043du0438u00a0 high orbit spacecraftthe u0438u0437u043cu0435u0440u0435u043du0438u00a0 angular velocity u0434u0432u0438u0436u0435u043du0438u00a0 orbital spacecraft, the first u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 time covered station orbit, block set u0438u00a0 moments of time u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 maximum power output of solar cells, the generator of time block u0441u0440u0430u0432u043du0435u043du0438u00a0 and key, and the second input unit u043eu043fu0440u0435u0434u0435u043bu0435u043du0438 u00a0 power is connected with the exit keyinformation and u0443u043fu0440u0430u0432u043bu00a0u044eu0449u0438u0439 entrances which are connected with the current sensor and the block u0441u0440u0430u0432u043du0435u043du0438u00a0 exits, respectively, first and second inlet which is connected with the exit ami respectively time generator and block u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 moments of time u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 maximum power output of solar cells.the first to fourth entrances which are connected to the outputs, respectively, of u0438u0437u043cu0435u0440u0435u043du0438u00a0 angle between the direction of the sun and the plane of the orbit space apt arata, block u0438u0437u043cu0435u0440u0435u043du0438u00a0 high orbit spacecraft, block u0438u0437u043cu0435u0440u0435u043du0438u00a0 angular velocity u0434u0432u0438u0436u0435u043du0438u00a0 orbital spacecraft and block u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 mo since the beginning of the orbit to be covered.
机译:系统 u043e u043f u0440 u0435 u0434 u0435 u043b u0435 u043d u0438 u00a0航天器太阳能电池板的最大功率输出 u0432 u043a u043b u044e u044e u0447 u0430 u044e u0449 u0430 u00a0太阳能电池,并在其 u0444 u043e u0442 u043e u044d u043d u043b u0435 u043a u0442 u0440 u0438 u0447 u0435 u0441 u0441 u0431 u043a u0438 u0445太阳能电池 u0443 u0441 u0438 u043b u0438 u0442 u0435 u043b u044c u043d u043e-转换设备,块 u0443 u043f u0440 u0430 u0432 u043b u0435 u043d u0438 u00a0太阳能电池在n方向上的方向和太阳块 u0440 u0435 u0433 u0443 u043b u00a0 u0442 u043e u0440 u043e u0432电流传感器,电流, u043e u043f u0440 u04340 u0435 u0434 u0435 u043b u0435 u043d u0438 u00a0供电 u0443 u043f u0440 u0430 u0432 u043b u0435 u043d u043d u0438 u00a0系统 u044d u043b u0435 u043a u0442 u0440 u043 u043d u0430 u0431 u0436 u0435 u043d u0438 u00a0和轮胎 u044d u043b u0435 u043a u0442 u0440 u043e u0441 u043d u0430 u0431 u04 36 u0435 u043d u0438 u00a0,其中出口块连接到块的入口 u0440 u0435 u0433 u0443 u043b u00a0 u0442 u043e u0440 u043e u0432 pv电源提示与夹板 u044d u043b u0435 u043a u0442 u0440 u043e u0441 u043d u04d u0430 u0431 u0436 u0435 u043d u0438d u00438 u00a0相连,并已将其与电流连接并锁定 u0435 u0434 u0435 u043b u0435 u043d u0438 u00a0电源并将输出单元连接到第一个 u0443 u043f u0440 u0430 u0432 u043b u0435 u043d u0438 u00a0系统 u044d u043b u0435 u043a u0442 u0440 u043e u0441 u043d u0430 u0431 u0436 u0435 u043d u0438 u00a0入口块 u0443 u043f u0440 u0430 u0432 u043b u0435 u043d u0438太阳能电池在太阳方向上的方向,直到哇与入口相连 u0443 u0441 u0438 u043b u0438 u0442 u0435 u043b u044c u043d u043e-与入口相连的转换设备太阳能电池的出口装置,其出口与第二入口模块 u0443 u043f u0440 u0430 u0432 u043b u0435 u043d u0438 u00a0太阳能电池在太阳,太阳能灯和设备的方向 u0435 u0445 u0430 u043d u0438 u0447 u0435 u0441 u043a u0438与太阳能电池电连接 u043e u0442 u043b u0438 u0447 u0430 u044e u0449 u0430 u00a0 u0441 u00a0,并添加了 u0438 u0437 u043c u0435 u0440 u0435 u043d u0438 u00a0太阳方向与轨道阱平面之间的角度 u0438 u0447 u0435 u0441 u043a u043e u0433 u043e设备,块 u0438 u0437 u043c u0435 u0440 u0435 u043d u0438 u00a0 u0438 u0437 u043c u0435 u0440 u0435 u043d u0438 u00a0角速度 u0434 u0432 u0438 u0436 u0435 u043d u0d轨道飞船,第一个 u043e u043f u0440 u0435 u0434 u0435 u043b u0435 u043d u0438 u00a0时间覆盖的站轨道,块集 u0438 u00a0时间时刻 u043e u043f u0440 u0435 u0434 u0435 u043b u0435 u043d u0438 u00a0最大输出功率o f个太阳能电池,时间块 u0441 u0440 u0430 u0432 u043d u0435 u043d u0438 u00a0和键的生成器,以及第二个输入单元 u043e u043f u0440 u0435 u0434 u0435 u043b u0435 u043d u0438 u00a0电源与退出键信息连接,并且 u0443 u043f u0440 u0430 u0432 u043b u00a0 u044e u0449 u0438 u0439入口与电流传感器和模块相连 u0441 u0440 u0430 u0432 u043d u0435 u043d u0438 u00a0分别退出,第一个和第二个入口分别与出口ami连接,时间发生器和块 u043e u043f u0440 u0435 u0434 u0435 u043b u0435 u043d u0438 u00a0时间的瞬间 u043e u043f u0440 u0435 u0434 u0435 u043b u0435 u043d u0438 u00a0与太阳能电池连接的第一至第四入口的最大功率输出。分别是 u0438 u0437 u043c u0435 u0440 u0435 u043d u0438 u00a0的输出,分别为 u0438 u0437 u0437 u043c u0435 u0440 u0435 u043d u0438 u00a0高轨道航天器,块 u0438 u0437 u043c u0435 u0440 u0435 u043d u0438 u00a0角速度 u0434 u0432 u0438 u0436 u0435 u043d u0438 u00438自要覆盖的轨道开始以来,轨道飞船和块 u043e u043f u0440 u0435 u0434 u0435 u043b u0435 u043d u0438 u00a0 mo。

著录项

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号