Method to control autonomous system of spacecraft power supply. RU patent 2521538.
|
Electric installation with electric battery capacity / 2520918 Invention refers to vehicle battery chargers. The presented electric installation with an electric battery capacity represents a power transmission facility comprising a voltage supply converter, an AC voltage network connected to an AC voltage terminal of the converter, and a DC voltage node connected to a DC voltage terminal of the converter. The converter comprises in-series connected switching elements each of which has at least one energy storage capacitor. The electric batteries can be parallel connected to the above capacitor, and a charging status can be adjusted by controlling the switching element of the voltage converter through a control circuit. |
|
Automotive transport power system with principle of periodic charging, discharging / 2520640 Invention relates to automotive transport power system with principle of periodic charging and discharging. Automotive transport power system contains automobile electric road, stations for electromobile charging and discharging, vehicle. Charging and discharging stations consist of control and monitoring unit, electric transformer, underground electric power cable, positive charge feed bus, negative charge feed bus, emergency generator. Charging stations are placed at uphills. Discharging stations are placed at downhills. Vehicle is active element. Vehicle contains automotive wheel base, electric motors, batteries, power-generating mechanism, recovery system, system for temporary storage and proper distribution of power. Electric current supply rod with rising-lowering mechanism is located on the bottom of vehicle. Charging and discharging is performed in motion. |
|
Charging system for electrical vehicles / 2520616 System contains at least one charging port with interface for energy exchange with at least one electrical vehicle, at least one power converter intended to convert power supplied from the power source such as the supply mains to the format suitable for the vehicle charging, at that the power converted is in remote position from the charging port, for example, in a separate room and/or building. |
 Monitoring system of electric power-driven tool, battery power source of electric power-driven tool, and charging device for batteries of electric power-driven tool / 2518520Application in the field of electrical engineering. The system includes a battery power source of electric power-driven tool and an auxiliary power supply source. The battery power source has a battery and a monitoring circuit. The battery has at least one battery cell. The monitoring circuit is actuated by electric power supplied from the battery; the circuit controls state of the battery. The auxiliary power supply source outputs electric power that allows operation of the monitoring circuit. The monitoring circuit is made so that when the circuit is inoperable with electric power supplied by the battery in result of battery voltage decrease the circuit may operate with electric power supplied by the auxiliary power supply source. |
 Power supply interface for electric tool powered by plurality of battery packs, and adapter / 2518518Electric tool containing tool case, electric load placed inside the above tool case; power supply interface for the above electric tool containing interface of the first battery pack adapted for removable fastening of the first battery pack and including an input terminal of the first battery positive terminal and an input terminal of the first battery negative terminal; interface of the second battery pack adapted for removable fastening of the second battery pack and including an input terminal of the second battery positive terminal and an input terminal of the second battery negative terminal. The input terminal of the first battery negative terminal is connected electrically to the input terminal of the second battery positive terminal, at that the input terminal of the first battery positive terminal is connected electrically the input terminal of the second battery negative terminal through the above electrical load. The indicators (160; 260) adapted for data display in regard to the respective states of the first battery packs are placed so that they are seen simultaneously by the electric tool user. |
 Hierarchical control system for battery of electric energy accumulators / 2518453Hierarchical control system for a battery of electric energy accumulators relates to the field of electric engineering and it can be used for manufacturing of high-voltage batteries of electric energy accumulators for transportation and power-generating sectors. The essence of the invention lies in that each of the series-connected electric energy accumulators has at its lower control level an individual control unit powered from the accumulator and connected at the medium control level through an intramodular serial communication channel isolated galvanically to the respective control unit of the electric energy accumulators powered and connected at the upper control level through an intramodular serial communication channel isolated galvanically with the battery control unit powered by the battery. The accumulator control unit consist of a monitoring and control unit based on a microcontroller and a balancing unit based on transformer circuit, which is made as a device for bidirectional energy transfer from an individual battery accumulator through a current sensor to the direct-current accumulating line end-to-end for the battery, this line contains parallel capacitors of the accumulator control units, which are coupled in parallel to secondary windings of the accumulative transformer made as a transformer with flyback voltage converter stepping the voltage up to the side of the battery accumulating line, with diodes shunted by electronic keys in the primary and secondary windings of the transformer and controlled from the respective drivers by means of the microcontroller for the accumulator control unit. The accumulator control unit is connected to the temperature control unit while the battery control unit based on the high-efficient microcontroller with enhanced memory capacity is connected to the battery current sensor, a switching unit with a fuse and onboard charge device and through in-series communication channel isolated galvanically to the onboard charge device and to external systems. |
 Accumulator battery (versions) and electric tool and accumulator battery assembly (versions) / 2515945Invention relates to an accumulator battery which is used as a power source for portable electric tools. The housing of the accumulator battery has a finger engaging portion which engages the finger(s) of an operator in the direction of removing the housing of the accumulator battery from the electric tool, a locking device capable of locking with the possibility of releasing the housing of the accumulator battery from the electric tool and a working element for unlocking the locking device. |
 Hierarchical three-level control system for high-voltage battery of electric energy accumulators / 2510658Invention relates to the field of electric engineering and it can be used for manufacturing of high-voltage batteries of electric energy accumulators for transportation and power-generating sectors. In the claimed device in accumulator control units at the low level of battery control besides available transformer channel of active selective balancing there's additional second choke channel of nearby balancing that allows intramodular balancing of accumulators charge under control of the control units at the low and medium control level and simultaneous intramodular balancing by means of transformer channel of selective balancing and accumulating line under control of the battery control unit at the upper control level. |
 Charging device / 2509401Charging device, comprising a unit of charging voltage release; a unit for setting of switching duration; a unit to generate a PWM signal; a unit to generate reference voltage; a unit to limit reference voltage; a unit to generate detected voltage; and a unit to control charging voltage. The unit to generate reference voltage generates reference voltage for detection of whether the charging voltage achieved the target charging voltage by means of smoothing of the PWM signal, generated from the unit of PWM signal discharge. The unit to limit reference voltage limits at least one of the maximum value or minimum value of reference voltage generated by the unit of reference voltage generation. |
 Charging system of electric power-driven tool, battery power source of electric power-driven tool, and charging device for batteries of electric power-driven tool / 2508592Each of the charging device for batteries and the battery power source has a microcomputer. Corresponding microcomputers jointly perform data exchange while the battery power source is charged by means of the charging device for batteries and confirm the working state of the microcomputer of the other side of data exchange (confirmation of interaction) based on the data exchange result. When malfunction of one of the microcomputers is detected, the other microcomputer performs a pre-defined process to stop the charging operation. |
 Automobile electrical system / 2244848Invention relates to energy accumulation systems using generator and storage and it is designed for use on vehicles with internal combustion engines. Proposed system contains electric motor, armature shaft of electric motor being designed for rotation of internal combustion engine shaft, first storage battery, first electromagnetic solenoid relay of electric motor, electric generator and battery switch. System is furnished also second storage battery, second and third electromagnetic relays, first and second magnetic contactors and selector switch with three contacts. First contacts of electric motor, switch, electric generator, windings of each contactor and each relay are connected with frame. Second contacts of winding of first magnetic contactor and first relay are connected with first fixed contact of selector switch. Second contacts of winding of second magnetic contactor, second and third electromagnetic relays are connected with second fixed contact of selector switch. First contacts of second and third magnetic relays and first magnetic contactor are connected with third movable contact of selector switch and with first pole of first battery. Second contacts of first and second magnetic contactors are connected with first pole of second battery. Second contact of electric motor is connected with first contact of first relay whose second contact is connected with second pole of second battery. Second contact of second relay is connected with second contact of first relay. Second contact of switch and first contact of second contactor are connected with second pole of first battery. Second contact of third relay is connected with second contact of generator. |
 High-speed cycling of storage-battery cells with enhanced current / 2284076Proposed method for high-speed cycling of battery cells with enhanced current includes battery filling with electrolyte, assembly of batteries in groups, their installation in liquid coolant filled reservoirs and settling-down, followed by multistage cycling with dc or pulse current. This treatment is effected in five stages; first stage involves passage of dc cycling current of 0.002-0.03Cn through battery for 10-60 minutes, its direction being reverse to normal one; during second stage current is reversed to normal and held within 0.002-0.03Cn for 10-60 minutes; third stage involves cycling with variable-polarity pulse current at charge pulse length of 100-300 s and discharge pulse length of 10-20 s, charge pulse amplitude being increased to 0.3-0.7Cn; fourth stage involves cycling for 1-3 h with variable-polarity pulse current at same length of charge and discharge pulses and constant amplitude of discharge pulses ranging between 0.3 and 0.7Cn; during fifth stage cycling is effected with variable-polarity pulse current and same length of charge and discharge pulses, amplitude of charge pulses being reduced to 0.15-0.4Cn; on-line control of third through fifth cycling stages is effected by using discharge pulses set up due to cell discharge across standard resistor as test ones and comparing their amplitude with experimental normalized amplitudes for each stage. Such procedure enables optimization of cycling lead-acid batteries with heavy current within short period at reduced in-process polarization of plates and their recharge, as well as enhancement of energy-intensive modification of β-PbO2 in positive-plate active material whose strength is also enhanced. |
 Computer-based production complex for cycling and charging flow-line produced storage batteries / 2287884Proposed computer-based production complex for cycling and charging flow-line produced storage batteries that incorporates provision for reducing mechanical damage to batteries during their loading in and removal from tanks under flow-line production conditions and for equalizing temperature gradients in tanks during battery cycling and charging has electrolyte holding machine, electrolyte level correcting machine, washing machine, degree-of-charge checking device, labeling machine, packing machine, hydraulic communication system with heat-transfer apparatus, set of power converters for feeding cycling and charging currents. Device for loading storage batteries on trays , device for removing batteries from trays, running cooling water tanks with movable controlled face walls are installed in line between two rail tracks with moving cars for trays mounting storage batteries. Battery-holding tray pushers and tanks are installed opposite inlet face walls of each tank. Guide rollers are disposed throughout entire length of each tank for moving trays incorporating slots uniformly arranged on surface and used for running water circulation. |
|
Method for accelerated charging of alkaline accumulators / 2293402 In accordance to method accumulators are charged with current impulses of different polarity with stabilized amplitudes of discharge and charge currents, while ratio of amplitudes of discharge and charge currents γ and ratio of durations of discharge and charge impulses τ are determined individually for each type of accumulators by means of two-factor experiment in intervals γ=1,1÷10 and τ=0,1÷0,9 respectively, amplitude of discharge current is calculated based on average current in accordance to required charging time, while charging time oscillates from 7 minutes to 4 hours depending on requirements of client, discharge process is stopped when voltage on accumulator reaches threshold value, charging of alkaline accumulators is performed in automatic mode without return of accumulators to original state. |
 Device for controlling accumulator charging / 2293415Device contains impulse generator, discharge chain circuit, indication circuit, outputs for connection of accumulator, key element, control circuit and source of direct stabilized voltage, to output of which connected electrically in parallel are impulse generator, first input of key element and also through smoothing filter - load, connected in parallel through discharge chain circuit are indication circuit and outputs of accumulator. New are introduced current limiting element, discharge key element, electrically connected to output of impulse generator, and launch circuit, input of which is electrically connected to outputs of discharge key element and control circuit, and output - to second input of key element, electrically connected by output to input of current-limiting element, another output of which is connected to inputs of control circuit, indication circuit and positive output of accumulator. |
 Autonomous voltage source / 2293416In autonomous voltage source, diode-capacitor block consists of capacitor, connected in parallel to photo-electric transformer, and two fast action Schottky diodes, first one of which is connected serially between photo-electric transformer and capacitor, and second one - between capacitor and accumulator battery on the side of its positive output. |
 Power supply turn-on and turn-off device / 2300166Proposed power turn-on and turn-of device has secondary power supply, code keying unit, control unit, actuating device with make contact, push-button with make contact, indicator, first and second input power buses, first and second output power buses. Novelty is introduction of code keying unit and new interconnections for functional components. |
 Method and device for restoring accumulator battery / 2309509Accumulator battery restoration method includes following modes and parameters - before beginning the restoration of accumulator battery, technological process parameters of accumulator battery restoration are recorded into memory of measuring device, which are compared in process of accumulator battery restoration to current values of accumulator battery restoration process parameters, which are corrected in case of deviation from given value of technological process parameters, charging of accumulator battery with constant current is stopped on achievement of given parameter values, recorded in the memory of measuring device, by current parameter values, after that accumulator battery is charged by letting a series of rectangular current impulses through it, duration of which impulses is set between 150 and 600 milliseconds, and pause between impulses ranges from 2 to 6 seconds, while amplitude of rectangular current impulses is kept unchanged at the temperature of electrolyte below predetermined value, and if the value of electrolyte temperature exceeds that value, the amplitude of rectangular current impulses is reduced to value, at which electrolyte temperature is reduced to predetermined value, and charging process is stopped on achievement of parameter values of measured values, defining end of battery charging process and recorded in the memory of measuring means in advance, after that battery capacity is measured by discharging it, which is stopped when battery voltage reaches limit value set for the battery, and accumulator battery restoration cycle is repeated, if capacity of the battery is less than 80% of nominal value. Device for restoring the accumulator battery contains block of charge current sources, output of which is used for connecting accumulator battery, current sensor, voltage sensor, temperature sensor, electrolyte density meter and memory block, it is fitted with processor, interface block, indication block and decoder, while memory block and indication block are connected to the processor, connected to which via interface block are current sensor, voltage sensor, temperature sensor and electrolyte density meter, processor output is connected to decoder input, first output of which is connected to input for controlling charging current source connection, and second output of decoder is connected to charging current parameter control input of charging current source block. |
 Method of accumulators charge with their grouping in system by principle of capacities division / 2329582Method of accumulators charge with their grouping in the system by principle of capacities division is characterised by the fact that accumulators are divided into groups that include single-type and close in value of their measured capacity accumulators, with equal number of serially connected accumulators in different groups. Groups are charges simultaneously and in parallel, from the same source that generates charging current, which is determined as sum of currents that are dependent on measured capacity of accumulators in groups. |
 Electric tooth bruch and disposable components / 2336846Invention concerns electric tooth brushes in which components of toothbrush heads are disposable. Electric tooth brush contains handle, head and waist, located between head and handle. Handle has internal hallow and head contains chaetas. Head contains at least one of components with electricity supply, interrupter, electrically connected to motor, located in internal hollow presented in handle. At least one component is connected by means of sliding connection with head of electric tooth brush, at that component can be detached or changed without detaching of components with electricity supply from mentioned tooth brush head. |
FIELD: electricity.
SUBSTANCE: invention is related to electric engineering and namely to power supply systems (PSS) of spacecraft using solar batteries as the primary energy sources and accumulator batteries as energy accumulators. The invention suggests a method for control of autonomous system of spacecraft power supply that contains a solar battery and n of accumulator battery, a voltage stabiliser coupled between the solar battery and load and n of charge and discharge devices; the method lies in control of the voltage stabiliser and charge and discharge devices depending on input and output voltage of the system, control of charge and discharge degree of the accumulator batteries, prohibition of operation for the respective charge device when it reaches the charge limit of the accumulator battery, enablement of operation when a certain discharge degree is reached by this accumulator battery, prohibition of operation for the respective discharge device when it reaches the discharge limit of the accumulator battery, enablement of operation when a certain charge degree is reached by this accumulator battery, at that in case when solar batteries loose their orientation to the Sun or in case of emergency discharge of accumulator batteries operation of all discharge devices is banned (locked), and after recovery of the solar batteries orientation to the Sun and charge of the accumulator batteries up to the preset level operation of all discharge devices is unlocked.
EFFECT: improvement of the PSS reliability in case of emergencies related to unscheduled loss of solar batteries orientation to the Sun.
3 cl, 2 dwg
The invention refers to electrical engineering, namely to power supply systems (SES) SPACECRAFT (SC), using as a primary energy sources solar batteries (SB), and as energy storage - rechargeable batteries).
Known way to control the Autonomous power supply system (patent RF №2059988, H02J 7/35)containing the solar battery (SA), a voltage regulator, connected between the solar battery and load, n batteries (n > 1), and "n" (AB) charge and discharge devices and for each AB - device control the degree of charge.
In the famous SES is carried out continuous control voltage, charge and discharge devices depending on the input (voltage SB) and output voltages SES. This charger ensures the battery charging, and a voltage regulator and a bit device can provide power to consumers.
Chain of continuous control (feedback) on the charger connected to the bus and SAT bus loads, a chain of continuous control voltage and discharge devices connected to the bus-load.
Depending on the degree of charge or discharge AB is a prohibition or permission charger works and discharge devices.
Such management provides longer operating SES. However, it does not provide fault tolerance SES when abnormal or emergency situations on the SPACECRAFT. In case of emergency, unplanned violations orientation of the SPACECRAFT solar Sun is a violation of the energy balance in the SES. If the loss of orientation will be prolonged, can be a total discharge of all AB. The onboard power consumers will then cease.
Known way to control the Autonomous power supply system (patent RF №2168828, H01J 7/36)containing the solar battery and n batteries, where n > 1, a voltage regulator, connected between the sun battery and load and n charge and discharge devices, consisting in the management of voltage and charge-discharge devices depending on the input and output voltage of the system, control level of charge and discharge batteries, ban the work of a proper charger when approaching extreme level a charge this battery pack, remove the ban on reaching a certain level of discharge this battery pack, the ban on the work of the relevant bit of the device when the limit level low battery charge this battery pack, remove the ban on reaching a certain level of charge this battery pack, characterized in that in case of loss of orientation of solar panels in the Sun, emergency battery discharge and disable parts bit device when the power remaining in the work of the bit devices is insufficient to power the load, prohibit all bit devices and voltage regulator, and stop running bit devices on signals about the condition of charge, then the danger of reverse polarity battery some batteries to it connect a device of protection of batteries against polarity reversal, after restoring the orientation of solar panels in the Sun at first make the batteries up to a certain amount of capacity, and then permit operation of the voltage regulator and resume control bit devices on signals about the condition of charge, the device protection of batteries against polarity reversal switch off after the beginning of the battery's charge.
This method is taken as a prototype of the claimed invention.
There is a method solves the problem of prevention of failure of battery AB, restore the normal functioning of the SES after abnormal or emergency situation.
However, the known method does not take into account the following fact. Currently, the SPACECRAFT have found wide application SES with several nominal output voltage. As a rule, it power system with parallel voltage regulator solar batteries (level 100 and more) and additional stabilization stress loads of smaller par value of tyres first load stable series converters. The structure of the SES reflected in the patent №2258292 EN dated 10 August 2005, according to which the power direct current from the source of limited power, such as solar panels, and the secondary source of electricity, for example batteries, is to stabilize the voltage on the load and the coordination of primary and secondary sources of electricity while stabilize n nominal voltage, and initially stabilize the voltage on the load, with a maximum supply voltage, and the voltage regulation of the remaining (n-1) loads carried out from power bus first load stable series converters, with the coordination of primary and secondary sources of electricity carried out only at the first level of the voltage and the voltage on the first level spend shunt or squirrel stabilized Converter.
For such SES famous invention requires a significant and fundamental improvements.
The task of the claimed invention is to increase the reliability of the SES at occurrence of emergency situations associated with an unplanned loss of orientation of the SPACECRAFT to the Sun.
The problem is solved by the fact that in the Autonomous power supply system of the spacecraft containing the solar battery and rechargeable n battery, voltage regulator, connected between solar and load and n charge and discharge devices, consisting in the management of voltage and charge-discharge devices depending on the input and output voltage of the system, control level of charge and discharge batteries, ban the work of a proper charger when approaching extreme level a charge this battery pack, remove the ban on reaching a certain level of discharge this battery pack, prohibition to work the corresponding bit device when approaching extreme level low battery charge this battery pack, remove the ban on reaching a certain level of charge this battery pack, while in case of loss of orientation of solar panels in the Sun, emergency battery discharge, prohibit(block) all bit devices, after restoring the orientation of solar panels in the Sun and charge the battery up to a specified level unlock all bit devices in power supply system with parallel voltage regulator solar panels and additional stabilization stress loads of smaller par value of tyres first load stable series converters are blocking the work of the data series stable converters, control the current solar panels, and releases the lock works stable series converters after exceeding the current solar panels pre-determined value. However, to block stable series converters removed after exceeding the current solar batteries values calculated from the ratio:
BS>(∑P SP /U SP +P ZAR /U ZAR )·n·k, where :
BS - current solar batteries; A;
P SP - power series stable Converter; W;
U SP - load voltage stable series Converter; W;
P ZAR - power for charging of accumulator batteries; W;
U ZAR minimum charging voltage; W;
n is the number of accumulator batteries;
k - coefficient of linefill (taking account of converters, etc.),
or the amount calculated based on the ratio:
BS>(∑P JV )k/U BS , where
BS-current solar panels, And;
P SP - power series stable Converter, W;
k - coefficient of linefill (taking account of converters, etc.);
U BS - rated voltage of the solar Century
At the discharge of each AB to the lower limit of this level AB is translated in storage mode.
After disabling the corresponding bit of the device power is remaining bit enabled devices from other AB, has not yet reached the specified level of discharge.
If after the ban multiple bit devices power remaining in the work of the JSB and the corresponding bit devices are not enough to ensure the supply side of consumers, prohibit all bit devices and stable series converters. The signal transition SES in storage mode can be, as well, reducing the voltage on the output tyres SES to a particular value (the lack of capacity of working bit devices output voltage SES begin to decline).
Accidental appearance of light SAT or restoring orientation SAT in the Sun and increasing the output voltage parallel stabilizer to the nominal value will be charging. You can unlock operation of the discharge devices and stable series converters. However, early inclusion series stabilized transducers can lead to the fact that the PV array voltage will remain at less than the nominal value (on the current-voltage characteristic is to the left of the voltage at the operating point) due to consumption Autonomous power supply system with no regulatory series converters (power transistors are completely open). This phenomenon is characteristic of SES with high output voltage (100 or more), when to get a high power use SAT with high voltage and proportionally less current (to reduce active power losses). Therefore, an effective solution here is to enable stable series converters at the current SAT sufficient to ensure as to charge the battery and to power consumers through a series voltage converters. This state operating point SB (close to the open-circuit voltage, or more precisely to the working point of maximum power). When used in power supply system of parallel voltage regulator solar cells have the ability to control the current SS even in the absence of load, as in this case, the entire current going through short regulatory transistor (after reaching the level of the stabilized voltage, for example 100).
Figure 2, shows the functional diagram of the Autonomous power supply system of the SPACECRAFT for the implementation of the proposed method which uses one stable series Converter for the organization of the second (lower, for example 27 In) voltage.
Autonomous power supply system KA contains a solar panel 1 with a current measuring shunt 1-1 in sub-zero circuit connected to a load of 2, and parallel voltage regulator 3 solar panels 1, rechargeable battery 4 1 -4 n , connected via charger 5 1 -5 n to a solar panel 1, and after a bit device 6 1 -6 n to the entrance to the output filter 23 voltage 3. In parallel to load 2 through a series of stabilized voltage Converter 20 connected to low voltage load 2-1.
In this case the load 2-1 in its composition contains the on-Board computer, system of the telemetry and command-measuring radio line (not shown).
Parallel with accumulator battery 4 1 -4 n connected device control batteries 7 1 -7 n associated entrance with storage batteries 4 1 -4 n to monitor the battery voltage and the output load 2-1.
In the chain of charge-discharge batteries installed measuring shunt -8 8 1 n .
Parallel voltage regulator consists of 3 short regulatory transistor 21, managed by the control circuit 22 and decoupling diode 23 in the plus bus SAT.
Charger 5 1 -5 n consist of control key 9, managed by the control circuit 10, booster unit, performed at the transformer 5-3, transistors 5-1 and 5-2 and rectifier diodes 5-4 and 5-5.
Bit device 6 1 -6 n consist of control key 11, managed by the control circuit 12.
Series stabilized voltage Converter consists of 20 control key 13, managed by the control circuit 14, input filter capacitor 15 and output filter on the diode 17, choke 18 and condenser 16.
Control circuit: 10 - chargers 5 1 -5 n , 12 - bit devices 6 1 -6 n 22 - parallel voltage 3 and 14 - series stabilized voltage Converter 20, made in the form of a pulse-width modulators, connected to the tyres of the stabilized voltage. Control circuits 10 chargers 5 1 -5 n optionally associated with measuring shunt -8 8 1 n and a load of 2.
Control sensor current 19 solar panels 1 connected entrance to the shunt 1-1 solar panels 1, and access to stable series Converter voltage 20.
The device works as follows. During operation rechargeable battery 4 1 -4 n work mainly in the storage and periodic dzarazov from solar panels 1 through charger 5 1 -5 n . Power 2 is thus the solar panels 1 through parallel voltage stabilizer 3, and load 2-1 through a series stabilized transmitter 20.
With the passage of the shadow of the orbit, or in violation of the orientation of duty 2 is powered by a rechargeable battery 4 1 -4 n through a bit device 6 1 -6 n .
Device control batteries 7 1 -7 n control voltage batteries rechargeable batteries 4 1 -4 n and transmit information about their condition in the load 2-1.
During operation KA, by results of the analysis of information on the state of the AB (mainly - voltage batteries and AB in General), logic hardware or planned in advance by the Board computer program is formed ban on all bit devices and stable series Converter.
After the restoration (partial or full) orientation of solar panels in the Sun after raising output voltage parallel stabilizer 3 to the nominal value is charged batteries. Banned bit device is removed after charging up to a certain level, and the ban on the work of the series stabilized voltage Converter 20 remove the sensor signal 19 current control SAT, after exceeding the current solar panels pre-determined value. The value of a preset value of a current security Council can be calculated from the ratio:
BS>(∑P SP /U SP +P ZAR /U ZAR )·n·k, where :
BS - current solar cells;
P SP - power series stable Converter;
U SP - load voltage stable series Converter;
P ZAR - power for charging of accumulator batteries;
U ZAR minimum charging voltage;
n is the number of accumulator batteries;
k - coefficient of linefill (taking account of converters, etc.) or based on the ratio:
BS>(∑P JV )k/U BS , where
BS - current solar panels, And;
P SP - power series stable Converter, W;
k - coefficient of linefill (taking account of converters, etc.);
U BS - rated voltage of the solar Century
Thus, the claimed method of management of the Autonomous power supply system of the spacecraft provides improved reliability SES at occurrence of emergency situations associated with an unplanned loss of orientation of the SPACECRAFT to the Sun.
1. The method of control of Autonomous power supply system of the spacecraft containing the solar battery and n battery, stabilizator voltage included between solar and load and n charge and discharge devices, consisting in the management of voltage and charge-discharge devices depending on the input and output voltage of the system, control level of charge and discharge batteries, ban the work of a proper charger when approaching extreme level a charge this battery pack, remove the ban on reaching a certain level of discharge this battery pack, the ban on the work of the relevant bit the device when approaching extreme level low battery charge this battery pack, remove the ban on reaching a certain level of charge this battery pack, while in case of loss of orientation of solar panels in the Sun, emergency battery discharge, prohibit (block) all bit devices, after restoring the orientation of solar panels in the Sun and charge the battery up to a specified level unlock all bit devices, characterized in that the electricity system with parallel stabilizer voltage solar panels and additional stabilization stress loads of smaller par value of tyres first load stable series converters are blocking the work of the data series stable converters, control the current solar panels, and releases the lock works stable series converters after exceeding the current solar panels pre-determined value.
2. The method of control of Autonomous power supply system of claim 1, characterized in that the block stable series converters removed after exceeding the current solar batteries values calculated from the ratio: BS>(∑P SP /U SP +P ZAR /U ZAR )·n·k, where I BS - current solar panels, And; P SP - power series stable Converter, W; U SP - load voltage stable series Converter, B; R ZAR - power for charging of accumulator batteries, W; U ZAR minimum charging voltage, W; n - number of batteries; k - the coefficient of linefill (taking account of converters, etc.).
3. The method of control of Autonomous power supply system of claim 1, characterized in that the block stable series converters removed after exceeding the current solar panels, calculated based on the ratio of: BS>(∑P JV )k/U BS where BS - current solar batteries, A; P SP - power series stable Converter, W; k - the coefficient of linefill (taking account of converters, etc.); U BS - rated voltage of the solar panels, B.