CN103699739A - Automatic designing and generating system for carrier rocket flight time sequence - Google Patents
Automatic designing and generating system for carrier rocket flight time sequence Download PDFInfo
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Abstract
The invention relates to an automatic designing and generating system for a carrier rocket flight time sequence, and belongs to the field of spacecraft electrical system automation design. Standard automatic output of the flight time sequence is achieved, the problem that manual design errors are easy to brought in when a sequence chart is drawn manually is avoided, and the design efficiency is improved; battery analysis and interpretation data automatic export functions are provided, so that the reliability of interpretation and reexamination is strengthened; management on the flight time sequence of rockets with different types, states and launching times is achieved through a database, the repeated work is reduced, and the control on the technical state change of the flight time sequence is achieved reasonably and effectively.
Description
Technical field
The present invention relates to a kind of carrier rocket flight sequential Automated Design and generation system, belong to spacecraft electrical system the Automation Design field.
Background technology
Carrier rocket flight timing Design needs a plurality of relevant specialities mutually to coordinate, require comprehensive trajectory result of calculation, standby guarantor's shutdown scheme, posture control system requirement, power system working routine, the requirement of separated sequential, control system circuit to realize and require (as power supply capacity executive capability, sequence equipment precision etc.), propellant utilization system, PUS to realize requirement (as the propellant utilization system, PUS open and close machine time) etc., feasible flight sequential reasonable in design.
Tradition flight timing Design pattern is that designer is manually depicted as the flight sequential designing the flight sequential chart of Auto CAD or Visio form, and sequential chart is exported to system designer, by system people, realizes flight sequential control.There is artificial interference factor in this design process, occurs that wrong probability is very high, and designer often needs repeatedly to check correctness and the consistance that just can guarantee between input and output.
For standard carrier rocket flight timing Design, Best available control technology state variation risk, shortens design cycle, strengthen interpretation and check reliability, improve design efficiency, avoiding people is the error causing, the sequential of accomplishing to fly is controlled to the overall process of flight validation from design source.
Summary of the invention
The object of the invention is for a kind of carrier rocket flight sequential Automated Design and production system are provided, by this system, having realized the standardization of flight sequential chart exports automatically, utilize the automatic export function of battery analysis and interpretation data, standard carrier rocket flight timing Design, shorten design cycle, strengthen interpretation and check reliability, improve design efficiency, avoiding people is the error causing, the sequential of accomplishing to fly is controlled to the overall process of flight validation from design source.
The object of the invention is to be achieved through the following technical solutions.
A kind of carrier rocket flight sequential Automated Design of the present invention and generation system, the functional module of this system comprises data management module, sequential chart drafting module, battery analysis module and data importing derivation module;
Data management module comprises that rocket model is managed, rocket is sent out inferior and a next state management, parameter and parameter type management, battery management, time series data management and active section management function;
Sequential chart drafting module comprises that AutoCAD sequential chart is drawn and Visio sequential chart is drawn;
Battery analysis module comprises amperometry and coulometric analysis function;
Data importing is derived module and is comprised that sequential list derivation, interpretation data derivation, time series data importing and derivation, supplemental characteristic import and export function.
Data management module provides a friendly operation interface for user, has realized the automatic management function that next state, parameter and parameter type, battery, time series data and active section were sent out time and sent out to different rocket models, rocket.
Sequential chart drafting module is produced the sequential chart of AutoCAD or Visio form automatically according to the time sequence information of user's typing, the step that sequential chart drafting module generates is automatically following a) to i) shown in:
A) from database, obtain all time series datas of this time;
B) travel through all sequential, the real time of calculating each sequential;
C) travel through all sequential, according to the reference sequential computing and plotting height of each sequential;
D) judge whether to draw according to the real time, if carry out f), carry out if not e);
E) travel through all sequential, according to each sequential real time, calculate the serial number of sequential;
F) draw zero point and transverse axis;
G) travel through all sequential, according to real time or serial number and the drawing number of plies, draw straight line and show control routine and the time;
Segment data while h) obtaining all working of this time from database;
I) traversal all working section, starts, finishes sequential and top number drafting straight line and show active section title according to active section.
Battery analysis module can be realized the amperometry of priming system and solenoid valve and the function that battery dump energy is analyzed, and by the automatic output current of form and the electric quantity curve of broken line graph, intuitively provide current peak and the battery dump energy of each sequential point, the performing step of battery analysis module is following a) to j) shown in:
A) from database, obtain all time series datas of this time;
B) from database, obtain selected battery information;
C) check data rationality, if unreasonable, finish battery analysis module, rationally carry out d);
D) whether interpretation draws coulometric analysis figure, if carry out e), otherwise carry out h);
E) travel through all sequential, the real time of calculating each sequential;
F) traversal sequential, calculates electric quantity change;
G) travel through all sequential, according to real time and electric weight drafting broken line graph;
H) travel through all sequential, the real time of calculating each sequential;
I) travel through all sequential, calculate curent change;
J) travel through all sequential, according to real time and electric current drafting broken line graph.
Beneficial effect
1, the standardization that has realized flight sequential is exported automatically, has avoided hand drawn sequential chart easily to introduce the problem of artificial design mistake, has improved design efficiency;
2, possess the automatic export function of battery analysis and interpretation data, strengthened the reliability of interpretation and check;
3, by database, realize different model, different conditions, the different flight timing management of sending out time rocket, reduce the duplication of labour, rationally effectively realize the management and control that flight sequential state of the art changes.
Accompanying drawing explanation
Fig. 1 is system function module composition diagram of the present invention;
The single carrier rocket flight of Fig. 2 sequential chart;
The different situations figure of Fig. 3 Time overlap;
The automatic product process figure of Fig. 4 sequential;
Fig. 5 battery automatic analysis process flow diagram;
In figure:
1, carrier rocket flight sequential Automated Design and generation system;
11, data management; 111, rocket model management; 112, rocket is sent out inferior and is sent out next state management, 113, parameter and parameter type and manage; 114, battery management; 115, time series data management; 116, active section management;
12, sequential chart is drawn; 121, AutoCAD sequential chart is drawn; 122, Visio sequential chart is drawn;
13, battery analysis; 131, amperometry; 132, coulometric analysis;
14, data importing is derived; 141, (Word) derived in sequential list; 142, interpretation data is derived (txt); 143, time series data is derived (Excel); 144, time series data imports (Excel); 145, supplemental characteristic is derived (txt); 146, supplemental characteristic imports (txt)
Embodiment
Below in conjunction with the drawings and specific embodiments, further illustrate feature of the present invention.
As shown in Figure 1, a kind of carrier rocket flight sequential Automated Design and production system 1, the functional module of this system comprises data management module 11, sequential chart drafting module 12, battery analysis module 13 and data importing derivation module 14;
Data management module 11 comprises that rocket model management 111, rocket send out time and send out next state management 112, parameter and parameter type management 113, battery management 114, time series data management 115 and active section management function 116;
Sequential chart drafting module 12 comprises the drafting 121 of AutoCAD sequential chart and Visio sequential chart drafting 122;
Battery analysis module 13 comprises amperometry 131 and coulometric analysis function 132;
Data importing derivation module 14 comprises sequential list derivation 141, interpretation data derivation 142, time series data importing 143 and time series data derivation 144, supplemental characteristic importing 145 and supplemental characteristic derivation 146.
Data management module realizes rocket model, rocket to send out time and send out next state, parameter and parameter type, battery data, time series data and active section data to be increased, delete, revises, inquires about, and simple checksum error prompt facility is provided.
Carrier rocket flight sequential Automated Design and production system, according to the data of inputting in data management module, are drawn out the sequential chart that standard is attractive in appearance automatically in AutoCAD, Visio software, and user can further adjust and revise sequential chart.Because whole rocket sequential quantity is more, there is multiple situation in the position of sequential, and some sequential need special processing etc.The process more complicated that the problems referred to above cause sequential chart to be drawn.
Single carrier rocket flight sequential comprises 5 lines+sequential code+sequential time, as shown in Figure 2.Because the time period forming with reference to sequential and sequential may occur to intersect with overlapping, during drawing, need to adopt different method for drafting for various situations.The modal situation of Time overlap as shown in Figure 3.The special processing that drafting sequential chart need to carry out is as follows:
1) overlapping sequential: during intersection, the height of sequential should be different, redundancy section will be removed when overlapping.
2) oneself height is different from the height when with reference to sequential: need consider to get extreme value simultaneously.
3) unused time and active section: color emphasizes, the timing shutdown time, (Td) needed special processing.
4) stochastic variable: stochastic variable is not drawn horizontal line and time.
By following steps, realize the calculating of timing curve:
Calculate absolute time → processing unused time information of all sequential → calculating branch information → traversal adjust height → traversal adjustment of the sequential of having intersected overlapping information → the drawing of order → evaluation work section of height → calculating sequential of sequential.
As shown in Figure 4, automatically generate the step of sequential chart of AutoCAD or Visio form following a) to i) shown in:
A) from database, obtain all time series datas of this time;
B) travel through all sequential, the real time of calculating each sequential;
C) travel through all sequential, according to the reference sequential computing and plotting height of each sequential;
D) judge whether to draw according to the real time, if carry out f), carry out if not e);
E) travel through all sequential, according to each sequential real time, calculate the serial number of sequential;
F) draw zero point and transverse axis;
G) travel through all sequential, according to real time or serial number and the drawing number of plies, draw straight line and show control routine and the time;
Segment data while h) obtaining all working of this time from database;
I) traversal all working section, starts, finishes sequential and top number drafting straight line and show active section title according to active section.
As shown in Figure 5, battery analysis module can be realized the amperometry of priming system and solenoid valve and the function that battery dump energy is analyzed, and by the automatic output current of form and the electric quantity curve of broken line graph, intuitively provide current peak and the battery dump energy of each sequential point, the performing step of battery analytic function is following a) to j) shown in:
A) from database, obtain all time series datas of this time;
B) from database, obtain selected battery information;
C) check data rationality, if unreasonable, finish battery analysis module, rationally carry out d);
D) whether interpretation draws coulometric analysis figure, if carry out e), otherwise carry out h);
E) travel through all sequential, the real time of calculating each sequential;
F) traversal sequential, calculates electric quantity change;
G) travel through all sequential, according to real time and electric weight drafting broken line graph;
H) travel through all sequential, the real time of calculating each sequential;
I) travel through all sequential, calculate curent change;
J) travel through all sequential, according to real time and electric current drafting broken line graph.
After timing Design completes, system can derive clear correct sequential list.In order to meet traditional expression way, need to carry out special processing to timing reference time, sequential working section and sequential decision time, unused time, random sequence etc., mainly comprise:
1) the reference sequential of sequential need change the sequential that the parameter type that is positioned at before this sequential is " unused time " into, and this need to analyze sequential computing time again globally.
2) derivation of sequential sequentially needs the while with reference to two factors of absolute time of the active section under sequential and sequential.
3) sequential that parameter type is " unused time " need to be carried out word overstriking, relative time changes the processing such as "/" into.
4) random sequential of time need to be carried out word overstriking, time and changed the processing such as "/" into, and the absolute time of all sequential with reference to this sequential need change the control routine of this sequential into.
The step that sequential list is derived is following a) to h):
A) traversal sequential, adds the arrow that represents on off operating mode to control routine;
B) traversal sequential, records all unused time by them according to time sequence;
C) travel through the unused time, determine the sequencing numbers of all unused time;
D) traversal sequential, determines sequencing numbers according to the reference sequential of sequential;
E) traversal sequential, recalculates relative time according to the sequencing numbers of sequential;
F) according to sequencing numbers and absolute time, sequential is sorted;
G) traversal sequential, carries out special processing to unused time sequential and random time sequential;
H) derived data.
Data importing is derived module and is comprised that sequential list derivation, interpretation data are derived, time series data imports and time series data is derived, supplemental characteristic imports and supplemental characteristic is derived.
The sequential list that can automatically produce word document form is derived in sequential list, and gauge outfit definition is shown in Table 1.
The gauge outfit of table 1 sequential list document
| Sequentially | 1 | 2 | 3 | 4 | 5 | 6 |
| Title | Step order | Explanation | Control code name | Remote measurement code name | Relative time | Absolute time |
Be described as follows:
A) step order: the sequential that absolute time is identical belongs to same step order, increases progressively successively since 1;
B) illustrate: the explanatory note of time sequence parameter;
C) control code name: the control routine of time sequence parameter;
D) remote measurement code name: the remote measurement code of time sequence parameter;
E) relative time: sequential is with respect to the previous time with reference to sequential, the sequential that the parameter type of usining during derivation is " unused time " is as with reference to sequential;
F) absolute time: the absolute time of sequential.
Time series data can export as the interpretation data of txt document format automatically, and the definition of document data form is shown in Table 2.
Table 2 interpretation data form
Be described as follows:
A) remote measurement code: the remote measurement code of time sequence parameter, in form, 1 is the remote measurement code of time sequence parameter, the 5th, with reference to the remote measurement code of time sequence parameter;
B) break-make symbol: " # " or " * ", wherein " # " represents to lead to, and " * " represents disconnected;
C) number of times: indicating time sequence parameter is which time occurs;
D) relative time: sequential is with respect to the previous time with reference to sequential, the sequential that the parameter type of usining during derivation is " unused time " is as with reference to sequential;
E) precision (just): the positive time precision of sequential;
F) precision (bearing): the negative time precision of sequential, during not enabled, absolute value equals positive time precision.
The importing of time series data and derivation, can import and derive Excel document time series data automatically.Document is divided into two pages of time series data and active section data, and the definition of time series data gauge outfit is shown in Table 3.
The gauge outfit of table 3 time series data
Be described as follows:
A) numbering: the numbering of sequential, has uniqueness;
B) control routine: the control routine of time sequence parameter;
C) Ref. No.: the numbering of the reference sequential of this sequential;
D) on off operating mode: the on off operating mode of sequential is that " breaking " duration is " TRUE ", and " leading to " duration is " FALSE ";
E) relative time: sequential is with respect to the time with reference to sequential;
F) precision (just): the time precision of sequential;
G) precision (bearing): the time precision of sequential, not enabled duration is 0, its absolute value of system default equals positive time precision;
H) random sequence; Whether be random sequence, when this sequential is that random sequence duration is " TRUE ", not for random sequence duration is " FALSE " if indicating this sequential;
I) battery: the battery title that sequential is used;
J) electric current: the electric current of sequential, unit: A;
K) level under: the affiliated level of sequential, " 1 " representative " core level ", " 2 " representative " boosting 13 ", " 3 " representative " boosting 24 ".
Supplemental characteristic imports and derives the supplemental characteristic of supporting txt document format, and the definition of document data form is shown in Table 4:
Table 4 supplemental characteristic form
Be described as follows:
A) parameter type: the parameter type title under parameter;
B) separator: for separating the character of attribute, be " # " here;
C) control routine: the control routine of parameter;
D) remote measurement code: the remote measurement code of parameter;
E) describe: the explanatory note of parameter.
Embodiment
The functional module of this carrier rocket flight sequential Automated Design and generation system comprises data management module, sequential chart drafting module, battery analysis module and data importing derivation module;
Data management module comprises that rocket model is managed, rocket is sent out inferior and a next state management, parameter and parameter type management, battery management, time series data management and active section management function;
Sequential chart drafting module comprises that AutoCAD sequential chart is drawn and Visio sequential chart is drawn;
Battery analysis module comprises amperometry and coulometric analysis function;
Data importing is derived module and is comprised that sequential list derivation, interpretation data derivation, time series data importing and derivation, supplemental characteristic import and export function.
Data management module provides operation interface for user, realizes the automatic management function that next state, parameter and parameter type, battery, time series data and active section were sent out time and sent out to different rocket models, rocket.
Sequential chart drafting module is produced the sequential chart of AutoCAD or Visio form automatically according to the time sequence information of user's typing;
Battery analysis module can be realized the amperometry of priming system and solenoid valve and the function that battery dump energy is analyzed, and by the automatic output current of form and the electric quantity curve of broken line graph, intuitively provides current peak and the battery dump energy of each sequential point.
The step that sequential chart drafting module generates is automatically following a) to j) shown in:
A) the flight time series data of a certain model rocket of typing, a certain state in data management module, flight sequential has several, the data message of single flight sequential comprises with reference to sequential, time of origin, time precision scope, and above-mentioned data are all kept in database;
B) draw the flight sequential chart of a certain state of a certain model rocket, all time series datas under this rocket flight state that needs to preserve in usage data storehouse, the rocket of take is zero point constantly, according to difference, with reference to sequential, calculate the actual time of origin of each sequential in rocket flight process, and sort according to the sequencing of time of origin;
C) corresponding each sequential, according to sequence successively, lines height, width, Digital size while calculating this sequential drafting according to the reference sequential of this sequential, guarantee that the situation of mutually blocking between sequential does not rationally appear in sequential spacing;
D) draw the time zero of flight sequential, draw the band horizontal line of arrow to the right, represent flight time axle;
E) select to draw according to the real time with respect to lift-off zero,take-off zero, or the sequencing occurring according to sequential is equidistantly drawn; If draw and carry out f according to the real time), carry out if not g);
F) travel through all sequential, according to real time and the drawing number of plies, draw straight line and show control routine and the time, then carry out h);
G) travel through all sequential, calculate the serial number of sequential according to each sequential real time, the serial number occurring according to sequential and the drawing number of plies are drawn straight line and are shown control routine and the time;
H) draw flight sequential working section: flight sequential working section is a set of sequential, several sequential that occur in certain a period of time in expression rocket flight process, for example rocket one-level inflight phase, secondary inflight phase all belong to flight sequential working section; In the database having recorded from data management module, segment data while obtaining all working of this time;
I) traversal all working section, starts, finishes sequential and top number drafting straight line and show active section title according to active section.
The performing step of battery analysis module is following a) to m) shown in:
Can a) the sequential power consumption data of a certain model rocket of typing, a certain state in data management module, meet the demands for analyzing the power consumption of rocket flight process battery.Comprise this type rocket battery numbering, the supply current data of all sequential, duration of power supply, supply current deviation range, and be kept in database;
B) from database, obtain all sequential power consumption data of this time;
C) from database, obtain selected battery number information, corresponding sequential supply current data;
D) check data rationality, if e is rationally carried out in the unreasonable work that stops carrying out battery analysis module);
E) whether interpretation draws coulometric analysis figure, if carry out f), otherwise carry out j);
F) all flight time series datas of storing in ergodic data administration module, calculate each flight sequential with respect to the actual time of origin of rocket lift-off zero,take-off zero;
G) take rocket lift-off zero,take-off zero as time reference, calculate the power consumption of each flight sequential, calculate the electric quantity change of battery in flight course;
H) take rocket lift-off zero,take-off zero as time reference, according to real time and electric weight drafting broken line graph;
I) complete coulometric analysis work;
J) take rocket lift-off zero,take-off zero as time reference, calculate the real time of each sequential;
K) take rocket lift-off zero,take-off zero as time reference, in data management module, inquire about the current data that each flight sequential consumes;
L) take rocket lift-off zero,take-off zero as time reference, the real time occurring according to each sequential and electric current are drawn broken line graph;
M) complete coulometric analysis work.
Claims (3)
1. carrier rocket flight sequential Automated Design and a generation system, is characterized in that: the functional module of this system comprises data management module, sequential chart drafting module, battery analysis module and data importing derivation module;
Data management module comprises that rocket model is managed, rocket is sent out inferior and a next state management, parameter and parameter type management, battery management, time series data management and active section management function;
Sequential chart drafting module comprises that AutoCAD sequential chart is drawn and Visio sequential chart is drawn;
Battery analysis module comprises amperometry and coulometric analysis function;
Data importing is derived module and is comprised that sequential list derivation, interpretation data derivation, time series data importing and derivation, supplemental characteristic import and export function;
Data management module provides operation interface for user, realizes the automatic management function that next state, parameter and parameter type, battery, time series data and active section were sent out time and sent out to different rocket models, rocket;
Sequential chart drafting module is produced the sequential chart of AutoCAD or Visio form automatically according to the time sequence information of user's typing;
Battery analysis module can be realized the amperometry of priming system and solenoid valve and the function that battery dump energy is analyzed, and by the automatic output current of form and the electric quantity curve of broken line graph, intuitively provides current peak and the battery dump energy of each sequential point.
2. a kind of carrier rocket flight sequential Automated Design according to claim 1 and generation system, is characterized in that: the step that sequential chart drafting module generates is automatically following a) to i) shown in:
A) from database, obtain all time series datas of this time;
B) travel through all sequential, the real time of calculating each sequential;
C) travel through all sequential, according to the reference sequential computing and plotting height of each sequential;
D) judge whether to draw according to the real time, if carry out f), carry out if not e);
E) travel through all sequential, according to each sequential real time, calculate the serial number of sequential;
F) draw zero point and transverse axis;
G) travel through all sequential, according to real time or serial number and the drawing number of plies, draw straight line and show control routine and the time;
Segment data while h) obtaining all working of this time from database;
I) traversal all working section, starts, finishes sequential and top number drafting straight line and show active section title according to active section.
3. a kind of carrier rocket flight sequential Automated Design according to claim 1 and generation system, is characterized in that: the performing step of battery analysis module is following a) to j) shown in:
A) from database, obtain all time series datas of this time;
B) from database, obtain selected battery information;
C) check data rationality, if unreasonable, finish battery analysis module, rationally carry out d);
D) whether interpretation draws coulometric analysis figure, if carry out e), otherwise carry out h);
E) travel through all sequential, the real time of calculating each sequential;
F) traversal sequential, calculates electric quantity change;
G) travel through all sequential, according to real time and electric weight drafting broken line graph;
H) travel through all sequential, the real time of calculating each sequential;
I) travel through all sequential, calculate curent change;
J) travel through all sequential, according to real time and electric current drafting broken line graph.
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Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106383969A (en) * | 2016-10-26 | 2017-02-08 | 北京宇航系统工程研究所 | Multi-body simulation data interaction method for launch vehicle |
| CN106595760A (en) * | 2016-12-08 | 2017-04-26 | 上海宇航系统工程研究所 | Design method for carrier rocket telemetry data automatic processing system |
| CN107862145A (en) * | 2017-11-13 | 2018-03-30 | 中国运载火箭技术研究院 | A kind of re-entry space vehicle flight time sequence and Energy Sources Equilibrium Coupling Design System and method for |
| CN108170900A (en) * | 2017-12-07 | 2018-06-15 | 北京空间技术研制试验中心 | Spacecraft firer ignites the method and simulation checking system of link simulation |
| CN109344499A (en) * | 2018-09-29 | 2019-02-15 | 中国航发哈尔滨轴承有限公司 | Rolling bearing engineering drawing method based on VB |
| CN109344084A (en) * | 2018-11-09 | 2019-02-15 | 北京空间技术研制试验中心 | The subsequent interpretation of spacecraft test data and criterion verification method |
| CN112130505A (en) * | 2020-09-27 | 2020-12-25 | 山东航天电子技术研究所 | Initiating explosive device ignition control circuit and method thereof |
| CN115077308A (en) * | 2022-05-18 | 2022-09-20 | 中国人民解放军61191部队 | Rocket space-time position simulation method and device based on rocket launching time sequence |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5522567A (en) * | 1994-12-28 | 1996-06-04 | Rockwell International Corp. | Energy management system for a gliding vehicle |
| CN101986318A (en) * | 2010-11-26 | 2011-03-16 | 南京航空航天大学 | Design method of concept prototype of flight control system |
| CN103090724A (en) * | 2013-01-21 | 2013-05-08 | 北京航空航天大学 | Solid-liquid power sounding rocket land launching sequential control system |
-
2013
- 2013-12-20 CN CN201310714272.3A patent/CN103699739B/en active Active
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5522567A (en) * | 1994-12-28 | 1996-06-04 | Rockwell International Corp. | Energy management system for a gliding vehicle |
| CN101986318A (en) * | 2010-11-26 | 2011-03-16 | 南京航空航天大学 | Design method of concept prototype of flight control system |
| CN103090724A (en) * | 2013-01-21 | 2013-05-08 | 北京航空航天大学 | Solid-liquid power sounding rocket land launching sequential control system |
Non-Patent Citations (2)
| Title |
|---|
| LI Y 等: "Neuro-controller design for nonlinear fighter aircraft maneuver using fully tuned RBF networks", 《AUTOMATICA》, 31 December 2001 (2001-12-31) * |
| 黄琼 等: "火箭时序参数判读方法分析与改进", 《飞行器测控学报》, vol. 32, no. 1, 28 February 2013 (2013-02-28) * |
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| CN106383969B (en) * | 2016-10-26 | 2019-08-09 | 北京宇航系统工程研究所 | A kind of carrier rocket multi-simulation data interactive method |
| CN106595760A (en) * | 2016-12-08 | 2017-04-26 | 上海宇航系统工程研究所 | Design method for carrier rocket telemetry data automatic processing system |
| CN107862145A (en) * | 2017-11-13 | 2018-03-30 | 中国运载火箭技术研究院 | A kind of re-entry space vehicle flight time sequence and Energy Sources Equilibrium Coupling Design System and method for |
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| CN109344084A (en) * | 2018-11-09 | 2019-02-15 | 北京空间技术研制试验中心 | The subsequent interpretation of spacecraft test data and criterion verification method |
| CN109344084B (en) * | 2018-11-09 | 2021-10-22 | 北京空间技术研制试验中心 | Spacecraft test data post interpretation and criterion verification method |
| CN112130505A (en) * | 2020-09-27 | 2020-12-25 | 山东航天电子技术研究所 | Initiating explosive device ignition control circuit and method thereof |
| CN115077308A (en) * | 2022-05-18 | 2022-09-20 | 中国人民解放军61191部队 | Rocket space-time position simulation method and device based on rocket launching time sequence |
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