CN112671083A - Multi-port converter circuit adapting to pulse load and control method thereof - Google Patents

Multi-port converter circuit adapting to pulse load and control method thereof Download PDF

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CN112671083A
CN112671083A CN202011427809.4A CN202011427809A CN112671083A CN 112671083 A CN112671083 A CN 112671083A CN 202011427809 A CN202011427809 A CN 202011427809A CN 112671083 A CN112671083 A CN 112671083A
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bus
voltage
super capacitor
converter circuit
storage battery
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朱洪雨
张博温
张艺
李林杰
邢浩江
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Shenzhen Aerospace New Power Technology Ltd
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Shenzhen Aerospace New Power Technology Ltd
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    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/50Photovoltaic [PV] energy
    • Y02E10/56Power conversion systems, e.g. maximum power point trackers

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Abstract

The invention provides a multi-port converter circuit adaptive to pulse load, which comprises a super capacitor CS, a solar array SA, a peak tracking system, a storage battery charging regulator, a storage battery discharging regulator and a bus, wherein the solar array SA is connected with the bus through the peak tracking system, the storage battery is connected with the bus through the storage battery charging regulator and the storage battery discharging regulator respectively, and the super capacitor CS is connected with the bus. The invention also provides a control method of the multi-port converter circuit adaptive to the pulse load. The invention has the beneficial effects that: the control mode of using super capacitor to adjust the bus directly uses the voltage at two ends of super capacitor as control signal, the battery charge and discharge and the bus control, thereby, the bus can respond the change of the load rapidly, and the problems of rapid fluctuation of the bus platform and poor quality of the primary bus brought by the pulse power type power load are avoided.

Description

Multi-port converter circuit adapting to pulse load and control method thereof
Technical Field
The invention relates to a satellite power supply system, in particular to a multi-port converter circuit adaptive to pulse load and a control method thereof.
Background
Satellite power systems play a crucial role throughout the operation of the satellite. It is the only power supply for the entire satellite platform and load. The stable operation of the satellite power supply system directly affects the service life of the whole satellite and the working condition of the satellite.
For the situation that the load fluctuation is large, such as the load is a pulse load, a laser, and the like, generally, the satellite power supply system cannot well cope with the load. At this moment, the bus of the satellite cannot be rapidly adjusted and balanced, and when the fluctuation is large, the influence on the working condition of the whole satellite is very serious. Therefore, how to better adapt to the pulse power load of the second level or the minute level and avoid the problems of the rapid fluctuation of the bus platform and the quality deterioration of the primary bus caused by the pulse power type power load is a technical problem to be solved urgently by those skilled in the art.
Disclosure of Invention
To solve the problems in the prior art, the present invention provides a multi-port converter circuit adapted to a pulse load and a control method thereof.
The invention provides a multi-port converter circuit adaptive to pulse load, which comprises a super capacitor CS, a solar array SA, a peak tracking system, a storage battery charging regulator, a storage battery discharging regulator and a bus, wherein the solar array SA is connected with the bus through the peak tracking system, the storage battery is connected with the bus through the storage battery charging regulator and the storage battery discharging regulator respectively, and the super capacitor CS is connected with the bus.
As a further improvement of the present invention, a bidirectional DC/DC converter is connected between the super capacitor CS and the bus.
As a further improvement of the invention, a PID regulator is connected between the bidirectional DC/DC converter and the bus.
The invention also provides a control method of the multi-port converter circuit adaptive to the pulse load, which is based on any one of the multi-port converter circuit adaptive to the pulse load to control the following steps:
and directly using the voltage Vcs at two ends of the super capacitor CS as a control signal to control the charging and discharging of the storage battery and the bus.
As a further improvement of the invention, the voltage Vcs at two ends of the super capacitor CS is used as a control signal to divide a control area, so that the storage battery enters a BCM charging area and a BDM discharging area, and the management of the charging and discharging of the battery is carried out.
As a further improvement of the invention, the voltage range of the super capacitor CS is close to the bus voltage.
As a further improvement of the invention, the voltage range of the super capacitor CS is between 70% and 95% of the steady state voltage value of the bus.
As a further improvement of the invention, the capacitance value C of the super capacitor CSSComprises the following steps:
Figure BDA0002825598140000021
desired pulse voltage VoutPulse current is IpDuration of tpDuring pulse formation, the voltage at the end of the storage capacitor is VcmaxDown to VcminThe conversion efficiency of the pulse forming topology is τ.
As a further improvement of the invention, the voltage range of the super capacitor CS is 70-95V, the steady state voltage value of the bus is 100V, and the voltage Vcs at two ends of the super capacitor CS is used as a control signal to ensure that the whole system works in the following different areas:
a) 85-95V, when the voltage value Vcs at two ends of the super capacitor CS is between 85-95V, the system (namely the satellite power supply system) works in the SUN domain, and at the moment, the solar array SA supplies power to the bus and charges the storage battery with constant maximum current;
b) the charging domain is 80-95V, and when the voltage value Vcs at two ends of the super capacitor CS is 80-85V, the storage battery is charged linearly;
c) and the discharge area is 70-80V, when the voltage value Vcs at two ends of the super capacitor CS is 70-80V, the storage battery discharges to supply power to the bus, and the solar array SA and the storage battery supply power to the bus simultaneously.
As a further improvement of the invention, the following control flows are carried out on the charging and discharging of the storage battery and the bus:
3) control of the SUN domain:
comparing the voltage value Vcs with a voltage value of a peak tracking system, taking a lower value, comparing with the current at the bus side, and performing PID control to be used as a control signal of an SUN domain;
4) and (3) battery charging and discharging management:
comparing the voltage value Vcs with the BCM battery management voltage, taking a higher value, comparing with the sampling of the inductive current of the battery, and performing PID control;
3) control of bus voltage:
and comparing the bus voltage sampling value with the reference value thereof for PID control, and controlling the bus voltage.
The invention has the beneficial effects that: the control mode of using super capacitor to adjust the bus directly uses the voltage at two ends of super capacitor as control signal, the battery charge and discharge and the bus control, thereby, the bus can respond the change of the load rapidly, and the problems of rapid fluctuation of the bus platform and poor quality of the primary bus brought by the pulse power type power load are avoided.
Drawings
Fig. 1 is a schematic diagram of a multi-port converter circuit adapted for pulsed loading in accordance with the present invention.
Fig. 2 is a control block diagram of a pulse load adaptive multiport converter circuit of the present invention.
FIG. 3 is a diagram of the operating region of a multi-port converter circuit adapted to a pulsed load according to the present invention
Fig. 4 is a schematic diagram of the SUN domain of a pulse load adaptive multiport converter circuit of the present invention.
Fig. 5 is a schematic diagram of the charge domain of a pulse load adaptive multiport converter circuit of the present invention.
Fig. 6 is a schematic diagram of the discharge domain of a pulse load adaptive multiport converter circuit of the present invention.
Fig. 7 is a SUN domain control diagram of a pulse load adaptive multiport converter circuit of the present invention.
Fig. 8 is a battery charge-discharge domain control diagram of a pulse load adaptive multi-port converter circuit of the present invention.
Fig. 9 is a busbar control diagram of a pulse load adaptive multiport converter circuit of the present invention.
Fig. 10 is a transient waveform diagram of a pulse load adaptive multiport converter circuit of the present invention.
Detailed Description
The invention is further described with reference to the following description and embodiments in conjunction with the accompanying drawings.
As shown in fig. 1 to 10, a multiport converter circuit adapted to an impulse load includes a super capacitor CS, a solar array SA, a peak tracking system (MPPT)101, a storage battery 104, a storage battery charging regulator 102, a storage battery discharging regulator 103, and a bus, where the solar array SA is connected to the bus through the peak tracking system 101, the storage battery 104 is connected to the bus through the storage Battery Charging Regulator (BCR)102 and the storage Battery Discharging Regulator (BDR)103, respectively, the super capacitor CS is connected to the bus, a bidirectional DC/DC converter 105 is connected between the super capacitor CS and the bus, a PID regulator 107 is connected between the bidirectional DC/DC converter 105 and the bus, and the bus is connected to a load 106.
A control method of a multi-port converter circuit adaptive to a pulse load adopts a control mode of a super capacitor to adjust a bus, and directly uses the voltage at two ends of the super capacitor as a control signal to control the charging and discharging of a battery and the bus. Thus, the BUS (BUS) can respond to the change of the load rapidly.
The solar array is connected with the bus through the MPPT (peak tracking system), and the MPPT controls the solar array SA (solar array) to output energy according to the power requirement of the spacecraft, so that the maximum output power of the solar array can be effectively exerted. The battery terminals are also directly connected to the bus bars. The voltage Vcs across the supercapacitor CS is used as a control signal to divide a control region, so that the battery (i.e., the storage battery 104) enters a BCM (battery charge management) charging region and a BDM (battery discharge management) discharging region, thereby managing the charging and discharging of the battery. The voltage Vcs across the super capacitor is connected with the load 106 through the bidirectional DC/DC converter 105, so that the dynamic response of the bus can be improved.
Selection of the super capacitor CS:
the function of the super capacitor CS is to quickly adjust the transient current load of the response bus. Since the energy stored by the capacitor is proportional to the square of the capacitor voltage, the voltage range of the supercapacitor CS is preferably chosen to be close to the bus voltage, so that the steady state voltage of the supercapacitor is taken to be 95V. Here a 3kw bi-directional DC/DC converter 105 with a super capacitor voltage range of 70-95V and a bus steady state voltage value of 100V.
Calculation of the capacitance value of the supercapacitor CS:
assuming the desired pulsed power supply is VoutPulse current is IpDuration of tpThen the energy required is at least:
Ep=Vout*Ip*tp
during pulse formation, the voltage at the end of the energy storage capacitor is VcmaxDown to VcminAssuming that the conversion efficiency of the pulse forming topology is τ, the following relationship exists:
Figure BDA0002825598140000061
obtained from the above formula:
Figure BDA0002825598140000062
because the pulse power is adjustable, and the pulse amplitude and the pulse duration are adjustable, the selection of the capacitor must be comprehensively considered by considering the maximum pulse energy and the maximum and minimum settings of the capacitor voltage, and the selection is usually larger.
One advantage of the invention is that by utilizing the characteristic that the super capacitor can be charged and discharged in a short time, when the bus has a large transient pulse current load, the voltage ripple caused by the action of the capacitor can be controlled to be small. The voltage Vcs at two ends of the super capacitor is used as a control signal, so that the whole system (namely a satellite power supply system) works in different areas.
a) SUN field 85-95V
As shown in fig. 4, when the voltage value Vcs across the super capacitor is between 85-95V, the system operates in the SUN domain, and at this time, the solar array supplies power to the bus while charging the battery at a constant maximum current.
b) Charging area of 80-95V
As shown in FIG. 5, the system charges the battery linearly when the voltage value Vcs across the super capacitor is 80-85V. The voltage value of each super capacitor corresponds to a battery charging current value. When the system enters the SUN domain, the system maintains a constant current value to charge the battery.
c) Discharge area of 70-80V
As shown in FIG. 6, when the voltage value Vcs of the super capacitor is between 70 and 80, the voltage provided by the solar array to the bus load is not enough to maintain the normal operation of the bus load. At this time, the battery discharge supplies power to the bus, and the solar array and the battery supply power to the bus at the same time.
The Vcs voltage is converted into a control signal after linear conversion through a differential circuit, and then PID control is carried out.
The control flow comprises the following steps:
1) control of the SUN domain:
as shown in fig. 7, Vcs is compared with MPPT, and after a lower value is obtained, PID control is performed as a control signal of the SUN domain by comparing with the bus-side current.
2) And (3) battery charging and discharging management:
as shown in FIG. 8, Vcs is taken high in comparison to the BCM battery management voltage. And comparing with the sample of the inductive current of the battery for PID control.
3) Control of bus voltage:
as shown in fig. 9, the BUS voltage sampling value is compared with the reference value thereof to perform PID control, and the BUS voltage is controlled. Therefore, the super capacitor can rapidly adjust the bus voltage.
As shown in fig. 10, when the bus has a 20A square wave pulse load, the impedance of the bus is maximized when the frequency of the load is increased to 1.4 KHz.
According to the multi-port converter circuit adaptive to the pulse load and the control method thereof, provided by the invention, by utilizing the characteristic that the super capacitor can be charged and discharged in a short time, when a bus has a large transient pulse current load, the voltage ripple caused by the action of the capacitor can be controlled to be very small.
The invention provides a multi-port converter circuit adaptive to a pulse load and a control method thereof, and provides a novel high-power supply controller with high power density, good load dynamic characteristics and low output impedance in order to adapt to second-level or minute-level pulse power loads.
The foregoing is a more detailed description of the invention in connection with specific preferred embodiments and it is not intended that the invention be limited to these specific details. For those skilled in the art to which the invention pertains, several simple deductions or substitutions can be made without departing from the spirit of the invention, and all shall be considered as belonging to the protection scope of the invention.

Claims (10)

1. A multi-port converter circuit adapted for pulsed loading, characterized by: the solar array SA is connected with the bus through the peak tracking system, the storage battery is connected with the bus through the storage battery charging regulator and the storage battery discharging regulator respectively, and the super capacitor CS is connected with the bus.
2. An impulse load compliant multiport converter circuit as recited in claim 1 wherein: and a bidirectional DC/DC converter is connected between the super capacitor CS and the bus.
3. An impulse load compliant multiport converter circuit as recited in claim 2 wherein: and a PID regulator is connected between the bidirectional DC/DC converter and the bus.
4. A method of controlling a multi-port converter circuit adapted for pulsed loading, the method comprising: the multi-port converter circuit for an impulsive load according to any one of claims 1 to 3, wherein:
and directly using the voltage Vcs at two ends of the super capacitor CS as a control signal to control the charging and discharging of the storage battery and the bus.
5. The method of controlling an impulse load compliant multiport converter circuit as recited in claim 4 wherein: and dividing a control area by taking the voltage Vcs at two ends of the super capacitor CS as a control signal, so that the storage battery enters a BCM charging area and a BDM discharging area, and managing the charging and discharging of the battery.
6. The method of controlling an impulse load compliant multiport converter circuit as recited in claim 4 wherein: the voltage range of the super capacitor CS is close to the bus voltage.
7. The method of controlling an impulse load compliant multiport converter circuit as recited in claim 4 wherein: the voltage range of the super capacitor CS is between 70% and 95% of the steady state voltage value of the bus.
8. According toThe method of controlling an impulse load compliant multiport converter circuit as recited in claim 4 wherein: capacitance value C of the super capacitor CSSComprises the following steps:
Figure FDA0002825598130000021
desired pulse voltage VoutPulse current is IpDuration of tpDuring pulse formation, the voltage at the end of the storage capacitor is VcmaxDown to VcminThe conversion efficiency of the pulse forming topology is τ.
9. The method of controlling an impulse load compliant multiport converter circuit as recited in claim 4 wherein: the voltage range of the super capacitor CS is 70-95V, the steady state voltage value of the bus is 100V, and the voltage Vcs at two ends of the super capacitor CS is used as a control signal to enable the whole multi-port converter circuit to work in the following different areas:
a) 85-95V, when the voltage value Vcs at two ends of the super capacitor CS is between 85-95V, the multi-port converter circuit works in the SUN domain, and at the moment, the solar array SA supplies power to the bus and charges the storage battery with constant maximum current;
b) the charging domain is 80-95V, and when the voltage value Vcs at two ends of the super capacitor CS is 80-85V, the storage battery is charged linearly;
c) and the discharge area is 70-80V, when the voltage value Vcs at two ends of the super capacitor CS is 70-80V, the storage battery discharges to supply power to the bus, and the solar array SA and the storage battery supply power to the bus simultaneously.
10. The method of controlling an impulse load compliant multiport converter circuit as recited in claim 4 wherein: the following control flows are carried out on the charging and discharging of the storage battery and the bus:
1) control of the SUN domain:
comparing the voltage value Vcs with a voltage value of a peak tracking system, taking a lower value, comparing with the current at the bus side, and performing PID control to be used as a control signal of an SUN domain;
2) and (3) battery charging and discharging management:
comparing the voltage value Vcs with the BCM battery management voltage, taking a higher value, comparing with the sampling of the inductive current of the battery, and performing PID control;
3) control of bus voltage:
and comparing the bus voltage sampling value with the reference value thereof for PID control, and controlling the bus voltage.
CN202011427809.4A 2020-12-09 2020-12-09 Multi-port converter circuit adapting to pulse load and control method thereof Pending CN112671083A (en)

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