CN103885418B - A kind of simulator dynamic control method based on delivery system - Google Patents

A kind of simulator dynamic control method based on delivery system Download PDF

Info

Publication number
CN103885418B
CN103885418B CN201410110706.3A CN201410110706A CN103885418B CN 103885418 B CN103885418 B CN 103885418B CN 201410110706 A CN201410110706 A CN 201410110706A CN 103885418 B CN103885418 B CN 103885418B
Authority
CN
China
Prior art keywords
simulator
computer
plc
control
output
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN201410110706.3A
Other languages
Chinese (zh)
Other versions
CN103885418A (en
Inventor
庄玮
蔡珂
向军
朱飞翔
吕振彬
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
SHANGHAI AEROSPACE COMPUTER TECHNOLOGY INSTITUTE
Original Assignee
Shanghai Aerospace Electronic Communication Equipment Research Institute
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Shanghai Aerospace Electronic Communication Equipment Research Institute filed Critical Shanghai Aerospace Electronic Communication Equipment Research Institute
Priority to CN201410110706.3A priority Critical patent/CN103885418B/en
Publication of CN103885418A publication Critical patent/CN103885418A/en
Application granted granted Critical
Publication of CN103885418B publication Critical patent/CN103885418B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P90/00Enabling technologies with a potential contribution to greenhouse gas [GHG] emissions mitigation
    • Y02P90/02Total factory control, e.g. smart factories, flexible manufacturing systems [FMS] or integrated manufacturing systems [IMS]

Landscapes

  • Testing And Monitoring For Control Systems (AREA)
  • Management, Administration, Business Operations System, And Electronic Commerce (AREA)

Abstract

The invention discloses a kind of simulator dynamic control method based on delivery system, first, simulator computer realizes the dynamic selection of selftest state by each order code word resolving main control computer;Secondly, described simulator computer, according to data protocol single between described simulator computer and simulator PLC, is sent to simulator PLC by the method for " one one meaning a, word one is worth " by having format, the control information of new content and output valve;Again, the control code that described simulator PLC sends by resolving described simulator computer dynamically controls mould and flies the DO output of simulator PLC described in output state real-time update;Finally, described simulator PLC is realized the dynamic control of AO output by the method for " one to one, one-to-many " by auxiliary reclay.Effectively simplify test condition and operation by this simulator dynamic control method, and improve testing efficiency and test motility, and decrease post personnel and manual operation.

Description

A kind of simulator dynamic control method based on delivery system
Technical field
The present invention relates to the technical field that general delivery system simulator controls, particularly relate to a kind of based on delivery system Simulator dynamic control method.
Background technology
Ground launch vehicle measurement is the important component part in delivery system.Carried out before launch vehicle measurement is delivered for use Simulator test directly examined function and the performance of this system.Optimization to simulator test can be effectively improved surveying a control The effect of system endurance.
In the prior art, existing equipment needs manually to recall the test panel of simulator computer in test process;Deng The AO output valve of effect device PLC is solidificated in PLC, it is impossible to enough changes in real time;And test event middle mold to fly state single, be merely able to into The long-time examination patterns of row, it is impossible to realize simulator system dynamics and control and meet high density carrier rocket launch mission to ground The high request of Test launch and control system.
Therefore, it is necessary to propose a kind of simulator dynamic control method based on delivery system, be effectively improved testing efficiency, Optimal inspection flow process meets the delivery system high requirement to ground Measure and launch system.
Summary of the invention
In order to overcome the defect of prior art, it is desirable to provide one is capable of initializing test panel, surveying Examination flow process, AO/DO, mould fly the dynamic control of the aspects such as pattern is various, and disclosure satisfy that highdensity carrier rocket launch mission Ground Test launch and control system is proposed the simulator dynamic control method based on delivery system of requirements at the higher level.
To achieve these goals, the invention provides a kind of simulator dynamic control method based on delivery system, should Simulator based on delivery system includes a simulator computer and simulator PLC, described simulator computer and described equivalence Connected by netting twine between device PLC, and between described simulator computer and external piloting control computer respectively by netting twine and RS232 cable connects, and by realizing the dynamic control to simulator connecting between each device, it specifically includes following step Rapid:
Step one: simulator computer realizes the dynamic of selftest state by each order code word resolving main control computer State selects;
Step 2: described simulator computer is according to data single between described simulator computer and simulator PLC Agreement, is sent to having format, the control information of new content and output valve by the method for " one one meaning a, word one is worth " Simulator PLC;
Step 3: the control code that described simulator PLC sends by resolving described simulator computer dynamically controls mould and flies The DO output of simulator PLC described in output state real-time update;
Step 4: described simulator PLC is realized AO output by the method for " one to one, one-to-many " by auxiliary reclay Dynamically control.
It is preferred that described step one farther includes: the simulator run on described simulator computer controls software and leads to Cross and resolve described main control computer and automatically recall the test surfaces of described simulator computer through the title code word that Transmission Control Protocol sends Plate;The simulator run on described simulator computer controls software by resolving what described master computer sent through Transmission Control Protocol Prompting code word is automatically into testing link accordingly;And the simulator run on described simulator computer controls software by resolving Described main control computer carries out testing the test of each passage in link through the control code word that RS232 cable sends automatically.
It is preferred that described step 2 includes: described simulator computer is resolving the life that good described main control computer sends After making code word, according to the data protocol between described simulator computer and described simulator PLC by control information and output valve Insert in a transmission array, then be sent to described simulator PLC by UDP;Wherein, described simulator computer and described equivalence Transmission rate between device PLC is 100ms/ frame.
It is preferred that described step 2 farther includes: the method for described " one one meaning a, word one is worth " is in packet The every bit of control code field represents different control code words or test event, and the every word of numerical value section represents different analog quantity numerical value.
It is preferred that described step 3 farther includes: described simulator PLC is receiving what described simulator computer sent After UDP frame, automatically resolve mould and fly mode bit, and fly the output of string output point when mode bit controls corresponding according to described mould;And institute State the information of each mode bit in simulator PLC real time parsing control code, be used for controlling corresponding DO output.
It is preferred that described step 4 farther includes: the pair of one is the corresponding centre of an analog output point Relay, the pair of mostly is the corresponding multiple analog datas of auxiliary reclay;And described simulator PLC is receiving UDP After frame, the value in data word is assigned in real time corresponding auxiliary reclay, thus realizes the dynamic control to AO output.
It is preferred that described auxiliary reclay is WORD type auxiliary reclay.
Compared with prior art, beneficial effects of the present invention is as follows:
1, the simulator dynamic control method based on delivery system of the present invention, mainly by debugging the most initial of panel Change and the dynamic response of testing process, the Protocol Design of " one one meaning a, word one is worth ", mould fly dynamically controlling and reality of state " one to one, one-to-many " auxiliary reclay dynamically controlled of existing AO output uses design, thus effectively achieves simulator The initialization of computer testing panel, testing process, AO/DO, mould fly the dynamic control of the aspects such as pattern is various, and disclosure satisfy that Highdensity carrier rocket launch mission ground Test launch and control system is had higher requirement the duration shorten, personnel Reduce, thus further increase analogue system to simplified system, raising testing efficiency and software optimization testing process, raising Coverage rate and the demand of state sneakerization.
2, the simulator dynamic control method based on delivery system of present invention design, by using " one one meaning, a word One value " the every bit of control code field in method for designing, i.e. packet represents different control code words or test event, numerical value section Every word represents different analog quantity numerical value;Owing to hardware upper part path is general, i.e. need in different test events Different conditions switches, and simulator computer software designs and was first emptied by data segment every time before sending Mode Control Code, then The simulator PLC, simulator PLC being sent in the lump behind the position 1 corresponding in the packet by PLC relay to be controlled Only need to by packet is 1 bit corresponding to relay connect and can realize, thus effectively reduce general time delay and wait Time, thus it is effectively improved efficiency.
3, the simulator dynamic control method based on delivery system of the present invention is by using fixing source, the most adjustable Mode flies state to mould and dynamically controls, and i.e. receives 422 code words that main control computer sends in test process, judges simultaneously This code word is that long mould flies instruction or short mould flies instruction, and shows in software shows the radio box at main interface, is finally receiving Take off signal time this state is sent to simulator PLC to realize mould is flown the dynamic regulation of state;Not only real by the method Show the dynamic regulation that mould is flown state, and decreased system post personnel and the operation of post personnel, mould has been flown simultaneously The polymorphic selection of state more achieves the target shortening test period, improving testing efficiency.
Accompanying drawing explanation
Fig. 1 is the system block diagram of present invention simulator based on delivery system;
Fig. 2 is the debugging panel dynamic initialization and the dynamic response flow chart of testing process that the present invention implements;
Fig. 3 is that " one one meaning a, word one is worth " agreement that the present invention implements uses program schematic diagram;
Fig. 4 is that the mould that the present invention implements flies state dynamic regulation logical flow chart;
Fig. 5 is that the auxiliary reclay that the analog output that the present invention implements dynamically controls uses program schematic diagram.
Symbol list:
10-main control computer;20-simulator based on delivery system, 21-simulator computer, 22-simulator PLC.
Detailed description of the invention:
See the accompanying drawing illustrating the embodiment of the present invention, the present invention hereafter be will be described in greater detail.But, the present invention can be with Multi-form, specification etc. realize, and should not be construed as the embodiment by herein proposing and limited.On the contrary, propose these to implement Example is to reach fully and complete disclosure, and makes the more model understanding the present invention about those skilled in the art completely Enclose.In these accompanying drawings, for clearly visible, relative size may be zoomed in or out.
The simulator dynamic control method based on delivery system implemented according to the present invention is described in detail referring now to Fig. 1, as Shown in Fig. 1, for the system structure of simulator based on delivery system, a simulator should be included by simulator 20 based on delivery system Computer 21 and simulator PLC22, connected by netting twine between this simulator computer 21 and simulator PLC22, and realization etc. When effect device controls, this simulator computer 21 is attached by netting twine and RS232 cable and a main control computer 10 respectively.
By the connection of this delivery system simulator, it realizes the concrete grammar step that simulator dynamically controls and includes:
Step one: simulator computer 21 realizes selftest state by each order code word resolving main control computer 10 Dynamic selection;Concrete, the simulator that this simulator computer 21 runs controls software by resolving this main control computer The 10 title code words sent through Transmission Control Protocol recall the test panel of this simulator computer 21 automatically;This simulator computer 21 The simulator of upper operation controls prompting code word that software sends through Transmission Control Protocol by resolving this main control computer 10 automatically into phase Link should be tested;And the simulator run on this simulator computer 21 controls software by resolving this main control computer 10 warp The control code word that RS232 cable sends carries out testing the test of each passage in link automatically;
Step 2: this simulator computer is assisted according to single data between simulator computer 21 and simulator PLC22 View, is sent to having format, the control information of new content and output valve by the method for " one one meaning a, word one is worth " Effect device PLC22;Concrete, this simulator computer 21 after resolving the order code word that this main control computer 10 good sends, according to Control information and output valve are inserted in a transmission array by the data protocol between simulator computer 21 and simulator PLC22, It is sent to simulator PLC22 again by UDP;Wherein, the transmission rate between this simulator computer 21 and simulator PLC22 is 100ms/ frame;
Step 3: the control code that this simulator PLC22 sends by resolving this simulator computer 21 dynamically controls mould and flies The DO output of output state real-time update this simulator PLC;Concrete, this simulator PLC22 is receiving the calculating of this simulator After the UDP frame that machine 21 sends, automatically resolve mould and fly mode bit, and fly the defeated of string output point when mode bit controls corresponding according to this mould Go out;And the information of each mode bit in this simulator PLC22 real time parsing control code, it is used for controlling corresponding DO output;
Step 4: this simulator PLC is realized the dynamic of AO output by the method for " one to one, one-to-many " by auxiliary reclay State controls;Concrete, it is the corresponding auxiliary reclay of an analog output point one to one, mostly is a middle relay for a pair The corresponding multiple analog datas of device;Value in data word, after receiving UDP frame, is assigned to accordingly by this simulator PLC22 in real time Auxiliary reclay, thus realize the dynamic control to AO output.
Wherein, the method being somebody's turn to do " one one meaning a, word one is worth " is that the every bit of control code field in packet represents different Controlling code word or test event, the every word of numerical value section represents different analog quantity numerical value;And in specific implementation process, continue in centre Electrical equipment is typically WORD type auxiliary reclay.
Practical example
In specific implementation process, debug the dynamic initialization of panel and the dynamic response stream of testing process as shown in Figure 2 Cheng Tu, this simulator computer 21, after receiving the tcp data frame that main control computer 10 sends, first determines whether according to frame format Whether it is title data, if title data, then continues to resolve the information in data bit, recall corresponding test surfaces according to this information Plate (is divided into the test events such as comprehensive, stable comprehensive, the general inspection of control);The display of test panel also illustrates this simulator computer 21 enter test mode;It follows that then to carry out dynamically according to the main control computer 10TCP Frame (prompting frame) received Flow process response (Switch operated by change of position test, servosystem test, one-level zero testing etc.), and carrying out dynamic flow process response Meanwhile, multithreading ground receives serial data (i.e. 422 control code), and resolves the implication of each control code thus carry out each lane testing (the F radio frequency channel test of servosystem, the test of H radio frequency channel, the test of G radio frequency channel, the test of HD radio frequency channel, the test of GD radio frequency channel and the F of appearance control electromagnetic valve + to G-lane testing etc.).
As it is shown on figure 3, be the use program example of " one one meaning a, word one is worth " method, in specific implementation process, One-level F1 lane testing in servosystem, in this test, it is desirable to the 4.5 of DO module of simulator PLC22,4.6,5.0,5.1 And the output port output 1 of 5.2, according to the data protocol between simulator computer 21 and simulator PLC22, for sending number In group Sdy_zt [] array, the 5th, 6 in the 11st byte and the 0th, 1,2 in the 12nd byte are set to 1, then by it Being sent to simulator PLC22, this simulator PLC22 only needs equally by between this simulator computer 21 and simulator PLC22 Data protocol resolves the information in this Frame, thus realizes the output of system requirements.
As shown in Figure 4, state dynamic regulation logic flow is flown, due in test process being embodied as embodiment middle mold Also having the serial data of extended formatting, so first carrying out the judgement of serial data type after entrance program, flying shape if mould State code word, then continue to judge data segment, if " FFFFFF ", then it represents that this time the mould of test flies state is that long mould flies, Now " the short mould flies " state box in simulator interface is shown as not choosing;If data segment is " 111111 ", then it represents that this time survey It is that short mould flies that the mould of examination flies state, and now in simulator interface, " short mould flies " state box is shown as choosing.And, specifically used During, this simulator computer, after receiving the signal that takes off that main control computer sends, reads the state of this state box, and will Send respective mode in UDP message frame to this simulator PLC22 to fly after mode bit is set to 1, to be sent to this simulator PLC22.Pass through This method to set up not only solves mould and flies the single immutable test pattern of state, and allows tester before take-off to mould Fly state dynamically to adjust, and while improving testing efficiency, add the motility of system test.
Such as Fig. 5 (a) to 5(b) it show the use program segment schematic diagram of auxiliary reclay, in specific implementation process, PLC Design require for an AO point can only unicoil output, export if carried out multi-coil then can cause exporting unsuccessful. And on simulator PLC hardware device same analog output point may different output parameters in corresponding multiple test events, as One rudder feedback UF is output, and on this simulator PLC hardware, the output port of distribution is PQW312, but in servosystem is tested In one-level, two grades and the test of three grades of servosystem different to this parameter request output valve, be respectively ± 1.4, ± 2.4 and ± 8.43, and servosystem requires that this port exports 0.45 in one-level zero testing, by simulator computer by numerical value and survey Examination project status write sends array Sdy_zt [] and is sent to simulator PLC, and this simulator PLC after receiving the data, presses Data protocol between simulator computer and simulator PLC resolves, and wherein, first determines whether test event (DB2.DBX3.2), Again the value of corresponding data code word (DB2.DBW31) is assigned to auxiliary reclay MW72 in real time;So, as long as by this auxiliary reclay Value be achieved that the dynamic control to analog output by the output of this port.
The simulator dynamic control method based on delivery system that the present invention provides mainly achieves test panel initial Change, testing process, AO/DO, mould fly the many dynamic control of pattern, and meet highdensity carrier rocket launch mission pair High request-the reduction of erection time of ground test launch control system offer, minimizing employee, thus further increase analogue system pair Simplified system, raising testing efficiency and software optimization testing process, raising coverage rate and the demand of state sneakerization.
Obviously, those skilled in the art can carry out various change and the deformation essence without deviating from the present invention to the present invention God and scope.So, if these amendments of the present invention and deformation belong to the scope of the claims in the present invention and equivalent technologies thereof In, then the present invention is also intended to comprise these changes.

Claims (4)

1. a simulator dynamic control method based on delivery system, it is characterised in that comprise the steps:
Step one: simulator computer realizes the dynamic choosing of selftest state by each order code word resolving main control computer Select;
Step 2: described simulator computer according to data protocol single between described simulator computer and simulator PLC, It is sent to equivalence by having format, the control information of new content and output valve by the method for " one one meaning a, word one is worth " Device PLC;
Step 3: the control code that described simulator PLC sends by resolving described simulator computer dynamically controls mould and flies output The DO output of simulator PLC described in state real-time update;
Step 4: described simulator PLC is realized the dynamic of AO output by the method for " one to one, one-to-many " by auxiliary reclay Control;
Described step one farther includes: the simulator run on described simulator computer controls software by resolving described master Control computer automatically recalls the test panel of described simulator computer through the title code word that Transmission Control Protocol sends;Described simulator The prompting code word that the simulator control software run on computer sends through Transmission Control Protocol by resolving described main control computer is automatic Enter and test link accordingly;And the simulator run on described simulator computer controls software and calculates by resolving described master control Machine carries out testing the test of each passage in link through the control code word that RS232 cable sends automatically;
Wherein, described " one one meaning a, word one is worth " method is that the every bit of control code field in packet represents different controls Code word processed or test event, the every word of numerical value section represents different analog quantity numerical value;
The pair of one is the corresponding auxiliary reclay of analog output point, the pair of mostly is an auxiliary reclay Corresponding multiple analog datas;And described simulator PLC is after receiving UDP frame, the value in data word is assigned in real time accordingly Auxiliary reclay, thus realize the dynamic control to AO output.
Simulator dynamic control method based on delivery system the most according to claim 1, it is characterised in that described step Two include: described simulator computer is after resolving the order code word that good described main control computer sends, according to described simulator Control information and output valve are inserted in a transmission array by the data protocol between computer and described simulator PLC, then pass through UDP is sent to described simulator PLC;Wherein, the transmission rate between described simulator computer and described simulator PLC is 100ms/ frame.
Simulator dynamic control method based on delivery system the most according to claim 1, it is characterised in that described step Three farther include: described simulator PLC, after receiving the UDP frame that described simulator computer sends, automatically resolves mould and flies shape State position, and fly the output of string output point when mode bit controls corresponding according to described mould;And described simulator PLC real time parsing controls The information of each mode bit in Ma, is used for controlling corresponding DO output.
Simulator dynamic control method based on delivery system the most according to claim 1, it is characterised in that described centre Relay is WORD type auxiliary reclay.
CN201410110706.3A 2014-03-24 2014-03-24 A kind of simulator dynamic control method based on delivery system Active CN103885418B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410110706.3A CN103885418B (en) 2014-03-24 2014-03-24 A kind of simulator dynamic control method based on delivery system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410110706.3A CN103885418B (en) 2014-03-24 2014-03-24 A kind of simulator dynamic control method based on delivery system

Publications (2)

Publication Number Publication Date
CN103885418A CN103885418A (en) 2014-06-25
CN103885418B true CN103885418B (en) 2017-01-04

Family

ID=50954366

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410110706.3A Active CN103885418B (en) 2014-03-24 2014-03-24 A kind of simulator dynamic control method based on delivery system

Country Status (1)

Country Link
CN (1) CN103885418B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106969674B (en) * 2017-05-03 2018-08-10 北京电子工程总体研究所 A kind of generalization ground checkout equipment based on PLC module

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101620261A (en) * 2009-07-23 2010-01-06 航天东方红卫星有限公司 Equivalent device for general satellite power-distribution system
CN101866178A (en) * 2010-06-18 2010-10-20 中国航天科技集团公司第五研究院第五一三研究所 Spacecraft equipment ground testing system and method
CN102809937A (en) * 2012-08-17 2012-12-05 上海航天测控通信研究所 PLC and 1553B based portable equivalent device for carrier rocket test-launch control system

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101620261A (en) * 2009-07-23 2010-01-06 航天东方红卫星有限公司 Equivalent device for general satellite power-distribution system
CN101866178A (en) * 2010-06-18 2010-10-20 中国航天科技集团公司第五研究院第五一三研究所 Spacecraft equipment ground testing system and method
CN102809937A (en) * 2012-08-17 2012-12-05 上海航天测控通信研究所 PLC and 1553B based portable equivalent device for carrier rocket test-launch control system

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
浅谈中间继电器的应用;陈敏栋;《机床电器》;20060212(第1期);第41-43页 *
飞行控制软件可靠性设计探讨;马卫华;《航天控制》;20020930(第3期);第77-81页 *

Also Published As

Publication number Publication date
CN103885418A (en) 2014-06-25

Similar Documents

Publication Publication Date Title
CN107769836B (en) Satellite universal automatic test platform and data interaction method thereof
CN106774260B (en) The automatic test approach and its system of on-board air conditioner controller
CN109521748B (en) Test method of unmanned vehicle
CN105892305B (en) General spacecraft ground tests bed system
CN106647335A (en) Digital satellite attitude and orbit control algorithm ground simulation verification system
CN110502430B (en) Flexible HIL test center and test method for vehicle electronic control unit
CN108227519A (en) CTCS2-200C type train control on board equipment automation simulation test platforms
CN105955067A (en) Multi-satellite intelligent cluster control simulation system based on quadrotor unmanned planes, and simulation method using the same to implement
CN105551088B (en) A kind of threedimensional model assembly and disassembly methods and device based on virtual group objects
CN104913942A (en) Detection system for automatic train operation system
CN103885418B (en) A kind of simulator dynamic control method based on delivery system
CN103412775A (en) Method for refreshing BMC firmware intelligently and automatically
CN107885186A (en) A kind of automatic test approach and system of automotive air-conditioning controller human-computer interaction function
CN104833825B (en) Light curtain target simulates check system
CN203881492U (en) Test system for automobile tire pressure sensor
CN110225100A (en) A kind of actual situation mapped system towards Intelligent assembly production line
CN105162655B (en) A kind of network throughput automated testing method and system
CN104834264A (en) PLC detection system and method of Railway carriage control chamber
CN106250623B (en) A kind of semi physical rapid simulation method steadily switched based on state
CN106406293B (en) A kind of engine controller automatic calibrating method
CN112749480B (en) Method for testing combination of bomb simulator and carrier
CN109901604A (en) A kind of aerostatics indoor sport control framework based on Matlab
CN115598972A (en) Pellet forming parameter control system, method, electronic device and storage medium
CN102540908B (en) General simulator for satellite attitude and track control subsystem closed-loop tests and method for general simulator
CN205375180U (en) Central test system of row accuse

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
TR01 Transfer of patent right
TR01 Transfer of patent right

Effective date of registration: 20180124

Address after: 200050 Anhua Road, Shanghai, No. 492, No.

Patentee after: SHANGHAI AEROSPACE COMPUTER TECHNOLOGY INSTITUTE

Address before: 200082 Qigihar Road, Shanghai, No. 76, No.

Patentee before: Shanghai Aerospace Electronic Communication Equipment Inst.