RU2013113430A - METHOD FOR CONTROLLING AN AUTONOMOUS POWER SUPPLY SYSTEM FOR THE SPACE VEHICLE - Google Patents
METHOD FOR CONTROLLING AN AUTONOMOUS POWER SUPPLY SYSTEM FOR THE SPACE VEHICLE Download PDFInfo
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- RU2013113430A RU2013113430A RU2013113430/07A RU2013113430A RU2013113430A RU 2013113430 A RU2013113430 A RU 2013113430A RU 2013113430/07 A RU2013113430/07 A RU 2013113430/07A RU 2013113430 A RU2013113430 A RU 2013113430A RU 2013113430 A RU2013113430 A RU 2013113430A
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Abstract
1. Способ управления автономной системой электроснабжения космического аппарата, содержащей солнечную батарею и «N» аккумуляторных батарей, где «N»≥1, стабилизатор напряжения, включенный между солнечной батареей и нагрузкой и «N» зарядных и разрядных устройств, заключающийся в управлении стабилизатором напряжения, зарядными и разрядными устройствами в зависимости от входного и выходного напряжения системы электроснабжения, напряжения аккумуляторных батарей, запрете на работу соответствующего зарядного устройства при достижении предельного уровня зарядного напряжения аккумуляторной батареи, либо ее аккумуляторов, снятии этого запрета при достижении определенного уровня напряжения аккумуляторной батареи, запрете на работу соответствующего разрядного устройства при достижении предельного уровня разрядного напряжения аккумуляторной батареи, либо ее аккумуляторов, снятии этого запрета при достижении определенного уровня напряжения аккумуляторной батареи, либо ее аккумуляторов, отличающийся тем, что устанавливают минимальный период времени достижения предельного уровня зарядного напряжения аккумуляторной батареи, либо ее аккумуляторов, от момента включения заряда, при этом, при включении заряда и достижении предельного уровня напряжения аккумуляторной батареи, либо ее аккумуляторов, в течение времени менее установленного минимального периода включают режим ограничения тока заряда по установленному уровню напряжения заряда аккумуляторной батареи.2. Способ управления автономной системой электроснабжения космического аппарата по п.1, отличающийся тем, что минимальный период времени достиж�1. A method for controlling an autonomous power supply system of a spacecraft containing a solar battery and “N” rechargeable batteries, where “N” ≥1, a voltage regulator connected between the solar battery and the load and “N” of charging and discharging devices, which consists in controlling the voltage stabilizer , charging and discharging devices, depending on the input and output voltage of the power supply system, the voltage of the batteries, the prohibition of the operation of the corresponding charger when reaching the pre an effective level of the charging voltage of the battery or its batteries, lifting this prohibition when a certain voltage level of the battery is reached, prohibiting the operation of the corresponding discharge device when reaching the maximum level of the discharge voltage of the battery, or its batteries, lifting this ban when a certain voltage level of the battery is reached battery, or its batteries, characterized in that they establish a minimum period of time to reach the maximum the level of the charging voltage of the rechargeable battery, or its batteries, from the moment the charge is turned on, and when the charge is turned on and the voltage level of the rechargeable battery or its batteries is reached, for less than a specified minimum period, the mode of charging current limitation to the set voltage level is activated battery charge 2. A method for controlling an autonomous power supply system of a spacecraft according to claim 1, characterized in that the minimum time period is reached
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RU2013113430/07A RU2541512C2 (en) | 2013-03-26 | 2013-03-26 | Method to control autonomous system of spacecraft power supply |
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RU2013113430/07A RU2541512C2 (en) | 2013-03-26 | 2013-03-26 | Method to control autonomous system of spacecraft power supply |
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RU2013113430A true RU2013113430A (en) | 2014-10-10 |
RU2541512C2 RU2541512C2 (en) | 2015-02-20 |
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RU2013113430/07A RU2541512C2 (en) | 2013-03-26 | 2013-03-26 | Method to control autonomous system of spacecraft power supply |
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Families Citing this family (3)
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US11396388B2 (en) | 2018-12-20 | 2022-07-26 | The Boeing Company | Optimized power balanced variable thrust transfer orbits to minimize an electric orbit raising duration |
US11401053B2 (en) * | 2018-12-20 | 2022-08-02 | The Boeing Company | Autonomous control of electric power supplied to a thruster during electric orbit raising |
US11753188B2 (en) | 2018-12-20 | 2023-09-12 | The Boeing Company | Optimized power balanced low thrust transfer orbits utilizing split thruster execution |
Family Cites Families (5)
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SU1148526A1 (en) * | 1983-12-09 | 1985-09-15 | Предприятие П/Я А-7449 | Apparatus for automatic monitoring of discharge of multicell storage battery |
US4880050A (en) * | 1988-06-20 | 1989-11-14 | The Boeing Company | Thermal management system |
US5036905A (en) * | 1989-10-26 | 1991-08-06 | The United States Of America As Represented By The Secretary Of The Air Force | High efficiency heat exchanger |
RU2313160C1 (en) * | 2006-03-22 | 2007-12-20 | Федеральное государственное унитарное предприятие "Научно-производственное объединение прикладной механики им. академика М.Ф. Решетнева" | Method for making nickel-hydrogen storage battery ready for full-time service in power supply system of artificial earth satellite |
RU2329572C1 (en) * | 2007-01-22 | 2008-07-20 | ФЕДЕРАЛЬНОЕ ГОСУДАРСТВЕННОЕ УНИТАРНОЕ ПРЕДПРИЯТИЕ "Научно-производственное объединение прикладной механики им. акадекмика М.Ф. Решетнева" | Method of operation of nickel-hydrogen accumulator battery |
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