CN105302993A - Automatic generation and dynamic display system for spacecraft power flow graph - Google Patents
Automatic generation and dynamic display system for spacecraft power flow graph Download PDFInfo
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- CN105302993A CN105302993A CN201510814648.7A CN201510814648A CN105302993A CN 105302993 A CN105302993 A CN 105302993A CN 201510814648 A CN201510814648 A CN 201510814648A CN 105302993 A CN105302993 A CN 105302993A
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- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F30/00—Computer-aided design [CAD]
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- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F30/00—Computer-aided design [CAD]
- G06F30/10—Geometric CAD
- G06F30/15—Vehicle, aircraft or watercraft design
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- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F30/00—Computer-aided design [CAD]
- G06F30/20—Design optimisation, verification or simulation
Abstract
The invention discloses an automatic generation and dynamic display system for a spacecraft power flow graph. The system comprises an IDS data import module, a layout and wiring module, a power flow calculation and display module and a power flow graph browse module. The IDS data import module is connected with the layout and wiring module and the power flow calculation and display module. The layout and wiring module and the power flow calculation and display module are connected with the power flow graph browse module. The power flow graph browse module is connected with the power flow calculation and display module. According to the automatic generation and dynamic display system, the spacecraft power flow graph is automatically generated in a standardized mode; compared with traditional power flow graph drawing steps, the problem that errors are introduced by manual drawing is avoided, the workload of a large graph designer is reduced, and the design efficiency is improved; data sources are unified, the spacecraft power supply and distribution large graph dynamic management function is achieved, changes of IDS data sources are automatically updated and reflected to the large graph, and therefore the full-task period spacecraft power supply and distribution condition is dynamically reflected in real time.
Description
Technical field
The present invention relates to spacecraft power flow chart generation technique field, be specifically related to a kind of spacecraft power flow chart and automatically generate and dynamic display system.
Background technology
The features such as spacecraft electrical system has System's composition complexity, and mission phase is many, and electric interfaces is complicated.Spacecraft has various combination state of flight at different mission phase, and under various combination state power supply-distribution system configuration and power flow direction inconsistent.In design phase, integration test stage, for reflecting better and grasping whole spacecraft power supply and distribution system duty and performance index, optimize power supply-distribution system design, need to carry out the design of spacecraft power flow chart.
Power flow chart embodies whole star power and produces, stores, regulates, transmits, distributes and user load quality event; Image characterizes the power flow direction of whole star for distribution; Embody the use (DC/DC of user load to bus; three-terminal voltage-stabilizing, directly to use), bus protection (switch relay, isolating diode, fuse, current-limiting resistance etc.), filtering circuit etc., in real time, dynamic response full duty cycle spacecraft power supply and distribution system poower flow situation.
Traditional power flow chart according to information such as system topological, device id S by designer, is drawn by computer software, is finally formed atlas.This design is mainly used in expressing the information such as power supply signal transmission path, and quantity of information is less, dynamically cannot represent poower flow relevant information; And standardization, readability are poor, impact examination, interchange and succession.
Summary of the invention
In order to solve the problem, the present invention aims to provide a kind of spacecraft power flow chart and automatically generates and dynamic display system, system emulation and analysis can be carried out to spacecraft power supply and distribution system poower flow, supplying Dynamic Announce simulation result parameter on the large figure of distribution, the distribution situation of electrical power flow to each load of power supply generation can be analyzed, and the change of the corresponding electrical quantities caused, there is provided spacecraft for distribution large figure dynamic management function, thus in real time, the full duty cycle spacecraft of dynamic response is for distribution situation.
For realizing above-mentioned technical purpose, reach above-mentioned technique effect, the present invention is achieved through the following technical solutions:
A kind of spacecraft power flow chart generates and dynamic display system automatically, comprises IDS data importing module, Placement and Routing module, poower flow calculate and display module and power flow chart browse module; Described IDS data importing module connects described Placement and Routing module respectively and described poower flow calculates and display module, described Placement and Routing module and described poower flow calculate and display module all browses model calling with described power flow chart, and described power flow chart is browsed module and to be calculated with described poower flow and display module is connected;
Described IDS data importing module reads the information in IDS management information system on IDS table respectively by IDS data importing means, and in cable system aided design system, cable junctions distributes the information in tables of data;
Described Placement and Routing module comprises Modulation recognition and filter element, equipment and connector layout units and harness wiring and adjusts functional unit;
Described Modulation recognition and filter element are according to category signal title, and self-defined signal type, realizes Modulation recognition; And realize wire filtration according to signal type;
Described equipment and connector layout units can make equipment, connector and contact according to the display of algorithm autoplacement, and provide multiple distributing adjustment instrument;
Described harness wiring and algorithm corresponding to adjustment functional unit, generate the wire of equipment room, complete wiring, and realize the adjustment in batches of wire;
Described poower flow calculates and display module passes through power calculation data, calculates the pressure drop at each equipment entrance place, and supports overload alarm;
Described power flow chart browses module support with Dynamic Graph mode visual expression power flow direction.
Further, the information on described IDS table comprises subsystem and stand-alone device relation on attributes; The information that described cable junctions is distributed in tables of data comprises cable connection relation information, cable length information and cable resistance information.
Further, described Modulation recognition and filter element can extract automatically according to conductor signal title rule, and on power flow chart, show primary power source type or secondary power supply type.
Further, described equipment and connector layout units possess following function:
1) equipment is according to algorithm autoplacement, and shows in units of subsystem;
2) connector is according to algorithm layout display on equipment;
3) contact is according to algorithm layout display on connector;
4) relation of inclusion of intelligent maintenance pel, is convenient to large figure rapid adjustment.
Further, described distributing adjustment instrument comprise aligned, rotate and supervisor inverted order.
Further, described harness wiring and adjustment functional unit possess following function:
1) according to global routing and the local wiring of automatic seeking footpath algorithm realization wire;
2) adjustment in batches of a branch of wire is realized according to wire adjustment algorithm;
3) relation of inclusion of intelligent maintenance pel, is convenient to large figure rapid adjustment.
The invention has the beneficial effects as follows:
The present invention can carry out system emulation and analysis to spacecraft power supply and distribution system poower flow, supplying Dynamic Announce simulation result parameter on the large figure of distribution, the distribution situation of electrical power flow to each load of power supply generation can be analyzed, and the change of the corresponding electrical quantities caused, there is provided spacecraft for distribution large figure dynamic management function, thus in real time, the full duty cycle spacecraft of dynamic response is for distribution situation.
The standardization that present invention achieves spacecraft power flow chart generates automatically, compared with traditional power flow chart plot step, present invention, avoiding the problem that manual drawing introduces mistake, decreases the workload of large G-Design teacher, improve design efficiency; The present invention has unified data source, and the change of IDS data source automatically can upgrade and be reflected to figure greatly.
Above-mentioned explanation is only the general introduction of technical solution of the present invention, in order to better understand technological means of the present invention, and can be implemented according to the content of instructions, coordinates accompanying drawing to describe in detail below with preferred embodiment of the present invention.The specific embodiment of the present invention is provided in detail by following examples and accompanying drawing thereof.
Accompanying drawing explanation
Accompanying drawing described herein is used to provide a further understanding of the present invention, and form a application's part, schematic description and description of the present invention, for explaining the present invention, does not form inappropriate limitation of the present invention.In the accompanying drawings:
Fig. 1 is system chart of the present invention and workflow diagram;
Fig. 2 is the definition schematic diagram of spacecraft power flow chart;
Fig. 3 is data source schematic diagram of the present invention.
Embodiment
Below with reference to the accompanying drawings and in conjunction with the embodiments, describe the present invention in detail.
Shown in Figure 1, a kind of spacecraft power flow chart generates and dynamic display system automatically, comprises IDS data importing module 1, Placement and Routing module 2, poower flow calculates and display module 3 and power flow chart browse module 4; Described IDS data importing module 1 connects described Placement and Routing module 2 respectively and described poower flow calculates and display module 3, described Placement and Routing module 2 calculates with described poower flow and display module 3 is all browsed module 4 with described power flow chart and is connected, and described power flow chart is browsed module 4 and to be calculated with described poower flow and display module 3 is connected.
Shown in Figure 2, spacecraft power flow chart forms by for distribution interface schema, equipment connecting relation and power calculation data three part, and these data sources then come from the IDS data importing shown in Fig. 3.
Further, shown in Fig. 1 and Fig. 3, described IDS data importing module 1 reads the information in IDS management information system 5 on IDS table 6 respectively by IDS data importing means, comprises subsystem and stand-alone device relation on attributes etc.; And the information read in cable system aided design system 7 in cable junctions distribution tables of data 8, comprise cable connection relation information, cable length information and cable resistance information etc.; Its specific implementation is as follows:
1) extract the annexation (contact level) between connector, contrast with IDS table 6, for the matching inspection of electrical connector plug and socket provides data source;
2) extract cable branch and length information thereof, provide data source for poower flow calculates.
Further, described Placement and Routing module 2 comprises Modulation recognition and filter element 21, equipment and connector layout units 22 and harness wiring and adjusts functional unit 23.
The specific works mode of described Modulation recognition and filter element 21 is as follows:
1) according to category signal title, self-defined signal type, realizes Modulation recognition;
2) realizing wire according to signal type to filter, as automatically extracted according to conductor signal title rule, and on power flow chart, showing primary power source type or secondary power supply type.
Described equipment and connector layout units 22 can make equipment, connector and contact according to the display of algorithm autoplacement, and provide multiple distributing adjustment instrument; Its specific works flow process is as follows:
1) equipment is according to algorithm autoplacement, and shows in units of subsystem;
2) connector is according to algorithm layout display on equipment;
3) contact is according to algorithm layout display on connector;
4) relation of inclusion of intelligent maintenance pel, is convenient to large figure rapid adjustment.
Described distributing adjustment instrument comprise aligned, rotate and supervisor's inverted order etc., device layout can be adjusted as required.
Described harness wiring and adjustment functional unit 23, according to the algorithm of correspondence, generate the wire of equipment room, complete wiring, and realize the adjustment in batches of wire; Its concrete function is as follows:
1) according to global routing and the local wiring of automatic seeking footpath algorithm realization wire; Spacecraft power flow chart can carry out the overall situation or local (cable connector, equipment, subsystem) self routing;
2) adjustment in batches of a branch of wire (cable branch) is realized according to wire adjustment algorithm; The Topology connection trend of cable head-end and end has a variety of, can adjust the wire trend of cable as required; Also can arrange cable/wire electrical properties (length, resistivity etc.); Power stage source point can also be set;
3) relation of inclusion of intelligent maintenance pel, is convenient to large figure rapid adjustment.
Further, described poower flow calculates and display module 3 passes through power calculation data, calculates the pressure drop at each equipment entrance place (power throttle point place), inspection poower flow each link derate situation, and supports overload alarm.
Further, described power flow chart is browsed module 4 and is expressed a bus and ground wire with bus form, with Dynamic Graph mode visual expression power flow direction.
Technical scheme of the present invention embodies whole star power and produces, stores, regulates, transmits, distributes and user load quality event; Image characterizes the power flow direction of whole star for distribution; Embody the use (DC/DC of user load to bus; three-terminal voltage-stabilizing, directly to use), bus protection (switch relay, isolating diode, fuse, current-limiting resistance etc.), filtering circuit etc., in real time, dynamic response full duty cycle spacecraft power supply and distribution system poower flow situation.
Meanwhile, the standardization that technical scheme of the present invention achieves spacecraft power flow chart generates automatically, compared with traditional power flow chart plot step, avoids the problem that manual drawing introduces mistake, decreases the workload of large G-Design teacher, improve design efficiency; Unified data source, the change of IDS data source automatically can upgrade and be reflected to figure greatly.
Above-described embodiment, just in order to technical conceive of the present invention and feature are described, its objective is and is one of ordinary skilled in the art can be understood content of the present invention and implement according to this, can not limit the scope of the invention with this.The change of every equivalence done by the essence of content of the present invention or modification, all should be encompassed in protection scope of the present invention.
Claims (6)
1. spacecraft power flow chart generates and a dynamic display system automatically, it is characterized in that: comprise IDS data importing module (1), Placement and Routing module (2), poower flow calculates and display module (3) and power flow chart browse module (4); Described IDS data importing module (1) connects described Placement and Routing module (2) respectively and described poower flow calculates and display module (3), described Placement and Routing module (2) calculates with described poower flow and display module (3) is all browsed module (4) and is connected with described power flow chart, and described power flow chart is browsed module (4) and to be calculated with described poower flow and display module (3) is connected;
Described IDS data importing module (1) reads the information in IDS management information system (5) on IDS table (6) respectively by IDS data importing means, and in cable system aided design system (7), cable junctions distributes the information in tables of data (8);
Described Placement and Routing module (2) comprises Modulation recognition and filter element (21), equipment and connector layout units (22) and harness wiring and adjusts functional unit (23);
Described Modulation recognition and filter element (21) are according to category signal title, and self-defined signal type, realizes Modulation recognition; And realize wire filtration according to signal type;
Described equipment and connector layout units (22) can make equipment, connector and contact according to the display of algorithm autoplacement, and provide multiple distributing adjustment instrument;
Described harness wiring and adjustment functional unit (23), according to the algorithm of correspondence, generate the wire of equipment room, complete wiring, and realize the adjustment in batches of wire;
Described poower flow calculating and display module (3), by power calculation data, calculate the pressure drop at each equipment entrance place, and support overload alarm;
Described power flow chart is browsed module (4) and is supported with Dynamic Graph mode visual expression power flow direction.
2. spacecraft power flow chart according to claim 1 generates and dynamic display system automatically, it is characterized in that: the information on described IDS table (6) comprises subsystem and stand-alone device relation on attributes; The information that described cable junctions is distributed in tables of data (8) comprises cable connection relation information, cable length information and cable resistance information.
3. spacecraft power flow chart according to claim 1 generates and dynamic display system automatically, it is characterized in that: described Modulation recognition and filter element (21) can extract automatically according to conductor signal title rule, and on power flow chart, show primary power source type or secondary power supply type.
4. spacecraft power flow chart according to claim 1 generates and dynamic display system automatically, it is characterized in that, described equipment and connector layout units (22) possess following function:
1) equipment is according to algorithm autoplacement, and shows in units of subsystem;
2) connector is according to algorithm layout display on equipment;
3) contact is according to algorithm layout display on connector;
4) relation of inclusion of intelligent maintenance pel, is convenient to large figure rapid adjustment.
5. spacecraft power flow chart according to claim 1 generates and dynamic display system automatically, it is characterized in that: described distributing adjustment instrument comprise aligned, rotate and supervisor inverted order.
6. spacecraft power flow chart according to claim 1 generates and dynamic display system automatically, it is characterized in that, described harness wiring and adjustment functional unit (23) possess following function:
1) according to global routing and the local wiring of automatic seeking footpath algorithm realization wire;
2) adjustment in batches of a branch of wire is realized according to wire adjustment algorithm;
3) relation of inclusion of intelligent maintenance pel, is convenient to large figure rapid adjustment.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201510814648.7A CN105302993B (en) | 2015-11-23 | 2015-11-23 | A kind of spacecraft power flow chart automatically generates and dynamic display system |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201510814648.7A CN105302993B (en) | 2015-11-23 | 2015-11-23 | A kind of spacecraft power flow chart automatically generates and dynamic display system |
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| CN105302993A true CN105302993A (en) | 2016-02-03 |
| CN105302993B CN105302993B (en) | 2018-12-14 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107103137A (en) * | 2017-04-26 | 2017-08-29 | 上海航天控制技术研究所 | A kind of design method of satellite control system cable system |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102999659A (en) * | 2012-11-13 | 2013-03-27 | 北京空间飞行器总体设计部 | Design method of dynamic power supply and distribution connection diagram |
| CN103176465A (en) * | 2013-03-28 | 2013-06-26 | 北京空间飞行器总体设计部 | Power supply and distribution test system for detector |
| US9171266B2 (en) * | 2008-10-15 | 2015-10-27 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Power provision based on self-sacrificing craft |
-
2015
- 2015-11-23 CN CN201510814648.7A patent/CN105302993B/en active Active
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9171266B2 (en) * | 2008-10-15 | 2015-10-27 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Power provision based on self-sacrificing craft |
| CN102999659A (en) * | 2012-11-13 | 2013-03-27 | 北京空间飞行器总体设计部 | Design method of dynamic power supply and distribution connection diagram |
| CN103176465A (en) * | 2013-03-28 | 2013-06-26 | 北京空间飞行器总体设计部 | Power supply and distribution test system for detector |
Non-Patent Citations (2)
| Title |
|---|
| 赵会光等: ""航天器精密设备隔振问题的功率流最优化研究"", 《宇航学报》 * |
| 赵会光等: ""航天器连接结构减振特性的功率流分析"", 《宇航学报》 * |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107103137A (en) * | 2017-04-26 | 2017-08-29 | 上海航天控制技术研究所 | A kind of design method of satellite control system cable system |
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