CN103984592A - Satellite instruction sequence processing method and device based on multiple tasks - Google Patents
Satellite instruction sequence processing method and device based on multiple tasks Download PDFInfo
- Publication number
- CN103984592A CN103984592A CN201410210694.1A CN201410210694A CN103984592A CN 103984592 A CN103984592 A CN 103984592A CN 201410210694 A CN201410210694 A CN 201410210694A CN 103984592 A CN103984592 A CN 103984592A
- Authority
- CN
- China
- Prior art keywords
- instruction
- instruction sequence
- satellite
- task
- identifying
- 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.)
- Granted
Links
Landscapes
- Radio Relay Systems (AREA)
Abstract
The invention discloses a satellite instruction sequence processing method and a satellite instruction sequence processing device based on multiple tasks. The method comprises the following steps that 1, all indirect instructions which are needed by remote control instruction tasks are obtained; 2, all the indirect instructions are encapsulated in the format of injection data with a corresponding amount to form an instruction sequence according to the maximum encapsulation value of each piece of injection data, wherein the instruction sequence comprises at least one instruction task; 3, all injection data in the instruction sequence are sent. According to the device and the method, the ground operation times are greatly reduced, the operation flow is simplified, the man-made misoperation is reduced, the reliability, the safety and the usability of the remote control operation are effectively improved; meanwhile, the ground operation time is shortened, the occupancy of the remote control resource is reduced, and the remote control efficiency is improved.
Description
Technical field
The present invention relates to aerospace measurement and control technology field, specifically, be a kind of high efficiencyly in the face of spacecraft program control in satellite instruction sequence disposal route and device based on multitask.
Background technology
The stored program control system that spacecraft is faced on ground generally has two kinds: indirect instruction mode and injecting data mode.Indirect instruction length is shorter, and its data field length is several crossed joints, is mainly the steering orders such as some units or application state switch, parameter arranges; The processing of indirect instruction comprises: produce, apply for sending, send, judge the processes such as implementation status, need many people to participate in a plurality of operations, the 6 second time of the shortest needs of processing of every indirect instruction.Injecting data length is longer, and the about hundreds of byte of its data field length, is mainly the longer data such as orbital data, almanac data, software code; The 8 second time of the shortest needs of processing of every injecting data of injecting data mode.Along with the function of satellite becomes increasingly complex, completing control task or load task needs many indirect instructions of a plurality of units to carry out successively according to certain flow process, some task need tens even hundreds and thousands of instructions according to certain flow process, carry out successively.At present, be all by ground, repeatedly to send indirect instruction to complete, existing indirect instruction one by one send mode is injected often, and spended time is long, need to expend a large amount of manpowers and channel resource, brings certain risk to the normal execution of task.
Summary of the invention
The object of the invention is to, a kind of satellite instruction sequence disposal route based on multitask is provided, can simplify ground straighforward operation, improve remote control resource utilization, improve reliability and the security of task.
For achieving the above object, the invention provides a kind of satellite instruction sequence disposal route based on multitask, comprise the following steps: (1) obtains all indirect instructions of telecommand required by task; (2) according to the maximum encapsulation value of every injecting data, all indirect instructions are encapsulated in the form of injecting data of respective number and form instruction sequence, wherein said instruction sequence comprises at least one instruction task; (3) send all injecting datas in described instruction sequence.
Further, described at least one instruction task comprises at least one injecting data, and described at least one injecting data comprises at least one indirect instruction.
Further, described instruction sequence form is: length: for identifying from validity field, start the total byte length finishing to assignment instructions list field; Type: the different instruction task type of carrying out for distinguishing satellite; Verification and: for identifying the cumulative sum verification that starts to finish to assignment instructions list field all bytes from validity field, only have verification just can carry out this instruction sequence via satellite; Validity: custom feature; Number of tasks: for identifying all instruction task quantity; Total instruction number: for identifying the total instruction number comprising when time instruction sequence; Mission bit stream: for identifying the corresponding initial order number information of all instruction tasks, every instruction task has two byte information; Assignment instructions list: detailed for identifying all instructions.Wherein, described number of tasks is from 1 open numbering.In described mission bit stream, the initial order of all instruction tasks numbering is from 1 open numbering, and the initial order of dummy instruction task numbering fixedly fills out 0.
Another object of the present invention, also provides a kind of satellite instruction sequence treating apparatus based on multitask, comprising: an instruction acquisition module, for obtaining all indirect instructions of telecommand required by task; One package module, be connected with described instruction acquisition module, for the form that all indirect instructions is encapsulated into the injecting data of respective number according to the maximum encapsulation value of every injecting data, form instruction sequence, wherein said instruction sequence comprises at least one instruction task; One sending module, is connected with described package module, for sending all injecting datas of described instruction sequence.
The invention has the advantages that, greatly reduce terrestrial operation number of times, simplified operating process, reduced human operational error, effectively improved reliability, security and the ease for use of straighforward operation; Reduce the terrestrial operation time simultaneously, reduced remote control resources occupation rate, improved remote control efficiency; And carry out by the duplication check of instruction sequence and the redundancy of instruction reliability and the security that has improved load task, there is stronger future in engineering applications, also can apply in the load task of other satellites or the remote control form of other complex task that needs many instructions cooperations.
Accompanying drawing explanation
Fig. 1, the process flow diagram of a kind of satellite instruction sequence disposal route based on multitask of the present invention;
Fig. 2 is instruction sequence form schematic diagram of the present invention;
Fig. 3, the Organization Chart of a kind of satellite instruction sequence treating apparatus based on multitask of the present invention.
Embodiment
Below in conjunction with accompanying drawing, a kind of satellite instruction sequence disposal route based on multitask provided by the invention and the embodiment of device are elaborated.
Shown in Figure 1, a kind of satellite instruction sequence disposal route based on multitask, comprises the following steps: S11: all indirect instructions of obtaining telecommand required by task; S12: according to the maximum encapsulation value of every injecting data, all indirect instructions are encapsulated in the form of injecting data of respective number and form instruction sequence, wherein said instruction sequence comprises at least one instruction task; S13: send all injecting datas in described instruction sequence.It is below the detailed description to above-mentioned steps.
S11: all indirect instructions of obtaining telecommand required by task.
By analysis, the instruction of satellite remote command required by task is indirect instruction, if indirect instruction is encapsulated in the form of injecting data, so every injecting data can hold many (for example 12) indirect instructions, this will improve observing and controlling segmental arc utilization factor greatly, and greatly reduce the complicacy of ground remote control operation.With existing satellite remote control form, be approximately decided to be example,, the longest 512 bytes of only supporting of complete remote control frame (being injecting data), and the byte information of every indirect instruction regulation is 29 bytes, add that corresponding packet header surrounds and command information, so the indirect instruction number that injecting data can encapsulate is at most 12.But in fact,, in practical application, if the byte information (29) of remote control frame length (512) and indirect instruction is all adjustable, the open ended indirect instruction quantity of injecting data is determined according to actual conditions.
S12: according to the maximum encapsulation value of every injecting data, all indirect instructions are encapsulated in the form of injecting data of respective number and form instruction sequence.
Because every injecting data can comprise many indirect instructions, therefore all indirect instructions of telecommand mission requirements can be packaged into one or more injecting data, form an instruction sequence and process; For example certain load task needs 12 indirect instructions, 12 indirect instructions is sequentially encapsulated in the form of an injecting data and forms an instruction sequence; The instruction of instruction sequence inside can be inserted each short instruction information dynamically, does not need permanent order, has greatly improved remote control efficiency.Also an instruction sequence comprises at least one instruction task, and an instruction task comprises at least one injecting data, and an injecting data comprises at least one indirect instruction.
With reference to figure 2, described instruction sequence form can comprise length, type, verification and, validity, number of tasks, total instruction number and assignment instructions list.
Wherein, length: start for identifying from validity field the total byte length finishing to assignment instructions list field, without unsigned int, account for 4B(byte);
Type: the different instruction task type of carrying out for distinguishing satellite, such as imaging, observation, data transmission etc., accounts for 2B;
Verification and: for identifying the cumulative sum verification that starts to finish to assignment instructions list field all bytes from validity field, only have verification just can carry out this instruction sequence via satellite, account for 2B;
Validity: be custom feature, can fixedly fill out 77H, account for 1B;
Number of tasks: for identifying all instruction task quantity, account for 1B, from 1 open numbering, each instruction sequence can comprise a plurality of instruction tasks;
Total instruction number: for identifying the total instruction number comprising when time instruction sequence, account for 2B, total instruction number maximal value depends on that spaceborne computer opens up the size to instruction sequence SRAM, and total instruction number span is 1 ~ 550;
Mission bit stream: for identifying the corresponding initial order number information of all instruction tasks, every instruction task has two byte information, wherein, the initial order of all instruction tasks is numbered from 1 open numbering, and the initial order of dummy instruction task numbering fixedly fills out 0;
Assignment instructions list: detailed for identifying all instructions, accounting for byte number is variable, and each indirect instruction comprises N byte information, packets of information is containing instruction time of each indirect instruction, order code, order parameter etc.
As shown in Figure 2, the mission bit stream of this instruction sequence comprises the initial order number information of 63 instruction tasks, from task 1 initial order numbering until task 63 initial order numberings.
Number of tasks herein and total instruction number are different concepts.In aforementioned, every injecting data can hold 12 indirect instructions and refers to, the remote control frame of 512 bytes holds at most 12 indirect instructions, and this is appointed by satellite remote control form; A satellite instruction task can be comprised of the instruction of 1 ~ n bar, and n cannot surpass total instruction number.And satellite has multiple-task for one day and needs to carry out, the efficiency of injecting in order to improve remote control, can be encapsulated in all instruction tasks instruction sequence the inside together, maximumly supports 63 instruction tasks, and the instruction number that all instruction tasks are added up is limited by total instruction number.
As shown in Figure 2, assignment instructions list comprises that instruction 1 is to instruction n information, and each indirect instruction comprises N byte information.N is the value that total instruction number is corresponding.
S13: send all injecting datas in described instruction sequence.
According to satellite remote control form agreement, all injecting datas in described instruction sequence are split into corresponding remote control frame, upper note, after satellite, then is assembled into a complete instruction sequence.Because every injecting data can comprise many indirect instructions, the transmission of therefore finishing the work by forming the form of instruction sequence, has reduced terrestrial operation number of times, has simplified operating process, reduce human operational error, effectively improved reliability, security and the ease for use of straighforward operation; Reduce the terrestrial operation time simultaneously, reduced remote control resources occupation rate, improved remote control efficiency; And carry out by the duplication check of instruction sequence and the redundancy of instruction reliability and the security that has improved load task, there is stronger future in engineering applications, also can apply in the load task of other satellites or the remote control form of other complex task that needs many instructions cooperations.
Illustrate, certain load task needs 12 instructions, carries out load task every day 14 times, at every turn must the upper note load task of 3 days.Table 1 has been listed traditional indirect instruction and the comparison of instruction sequence of the present invention aspect transmitting time, transmission times, wherein, and 6 second time of the shortest needs of the processing of every indirect instruction, the 8 second time of the shortest needs of processing of every injecting data.By following table, relatively can find out, obviously the transmission times of instruction sequence of the present invention and transmitting time are much smaller than traditional indirect instruction mode, and efficiency improves greatly.
| Sequence number | Performance | Tradition indirect instruction | Instruction sequence of the present invention |
| 1 | Transmitting time (S) | 3024 | 336 |
| 2 | Transmission times | 504 | 42 |
The Performance Ratio of the traditional indirect instruction of table 1 and instruction sequence.
With reference to figure 3, a kind of satellite instruction sequence treating apparatus based on multitask of the present invention, comprising: an instruction acquisition module 31, a package module 32 and a sending module 33.
Described instruction acquisition module 31, for obtaining all indirect instructions of telecommand required by task.By analysis, the instruction of satellite remote command required by task is indirect instruction, if indirect instruction is encapsulated in the form of injecting data, so every injecting data can hold many (for example 12) indirect instructions, this will improve observing and controlling segmental arc utilization factor greatly, and greatly reduce the complicacy of ground remote control operation.
Described package module 32 is connected with described instruction acquisition module 31, for the form that all indirect instructions is encapsulated into the injecting data of respective number according to the maximum encapsulation value of every injecting data, forms instruction sequence.Because every injecting data can comprise many indirect instructions, therefore all indirect instructions of telecommand mission requirements can be packaged into one or more injecting data, form an instruction sequence and process.The instruction of instruction sequence inside can be inserted each short instruction information dynamically, does not need permanent order, has greatly improved remote control efficiency.Also an instruction sequence comprises at least one instruction task, and an instruction task comprises at least one injecting data, and an injecting data comprises at least one indirect instruction.
Described instruction sequence form can comprise length, type, verification and, validity, number of tasks, total instruction number and assignment instructions list, specifically with reference to shown in figure 2.
Wherein, length: start for identifying from validity field the total byte length finishing to assignment instructions list field, without unsigned int, account for 4B(byte);
Type: the different instruction task type of carrying out for distinguishing satellite, such as imaging, observation, data transmission etc., accounts for 2B;
Verification and: for identifying the cumulative sum verification that starts to finish to assignment instructions list field all bytes from validity field, only have verification just can carry out this instruction sequence via satellite, account for 2B;
Validity: be custom feature, can fixedly fill out 77H, account for 1B;
Number of tasks: for identifying all instruction task quantity, account for 1B, from 1 open numbering, each instruction sequence can comprise a plurality of instruction tasks;
Total instruction number: for identifying the total instruction number comprising when time instruction sequence, account for 2B, total instruction number maximal value depends on that spaceborne computer opens up the size to instruction sequence SRAM, and total instruction number span is 1 ~ 550;
Mission bit stream: for identifying the corresponding initial order number information of all instruction tasks, every instruction task has two byte information, wherein, the initial order of all instruction tasks is numbered from 1 open numbering, and the initial order of dummy instruction task numbering fixedly fills out 0;
Assignment instructions list: detailed for identifying all instructions, accounting for byte number is variable, and each indirect instruction comprises N byte information, packets of information is containing instruction time of each indirect instruction, order code, order parameter etc.
Described sending module 33 is connected with described package module 32, for sending all injecting datas of described instruction sequence.According to satellite remote control form agreement, all injecting datas in described instruction sequence are split into corresponding remote control frame, upper note, after satellite, then is assembled into a complete instruction sequence.Because every injecting data can comprise many indirect instructions, the transmission of therefore finishing the work by forming the form of instruction sequence, has reduced terrestrial operation number of times, has simplified operating process, reduce human operational error, effectively improved reliability, security and the ease for use of straighforward operation; Reduce the terrestrial operation time simultaneously, reduced remote control resources occupation rate, improved remote control efficiency; And carry out by the duplication check of instruction sequence and the redundancy of instruction reliability and the security that has improved load task, there is stronger future in engineering applications, also can apply in the load task of other satellites or the remote control form of other complex task that needs many instructions cooperations.
The above is only the preferred embodiment of the present invention; it should be pointed out that for those skilled in the art, under the premise without departing from the principles of the invention; can also make some improvements and modifications, these improvements and modifications also should be considered as protection scope of the present invention.
Claims (10)
1. the satellite instruction sequence disposal route based on multitask, is characterized in that, comprises the following steps:
(1) obtain all indirect instructions of telecommand required by task;
(2) according to the maximum encapsulation value of every injecting data, all indirect instructions are encapsulated in the form of injecting data of respective number and form instruction sequence, wherein said instruction sequence comprises at least one instruction task;
(3) send all injecting datas in described instruction sequence.
2. the satellite instruction sequence disposal route based on multitask according to claim 1, is characterized in that, described at least one instruction task comprises at least one injecting data, and described at least one injecting data comprises at least one indirect instruction.
3. the satellite instruction sequence disposal route based on multitask according to claim 1, is characterized in that, described instruction sequence form is:
Length: start the total byte length finishing to assignment instructions list field for identifying from validity field;
Type: the different instruction task type of carrying out for distinguishing satellite;
Verification and: for identifying the cumulative sum verification that starts to finish to assignment instructions list field all bytes from validity field, only have verification just can carry out this instruction sequence via satellite;
Validity: custom feature;
Number of tasks: for identifying all instruction task quantity;
Total instruction number: for identifying the total instruction number comprising when time instruction sequence;
Mission bit stream: for identifying the corresponding initial order number information of all instruction tasks, every instruction task has two byte information;
Assignment instructions list: detailed for identifying all instructions.
4. the satellite instruction sequence disposal route based on multitask according to claim 1, is characterized in that, described number of tasks is from 1 open numbering.
5. the satellite instruction sequence disposal route based on multitask according to claim 1, is characterized in that, in described mission bit stream, the initial order of all instruction tasks numbering is from 1 open numbering, and the initial order of dummy instruction task numbering fixedly fills out 0.
6. the satellite instruction sequence treating apparatus based on multitask, is characterized in that, comprising:
One instruction acquisition module, for obtaining all indirect instructions of telecommand required by task;
One package module, be connected with described instruction acquisition module, for the form that all indirect instructions is encapsulated into the injecting data of respective number according to the maximum encapsulation value of every injecting data, form instruction sequence, wherein said instruction sequence comprises at least one instruction task;
One sending module, is connected with described package module, for sending all injecting datas of described instruction sequence.
7. the satellite instruction sequence treating apparatus based on multitask according to claim 6, is characterized in that, described at least one instruction task comprises at least one injecting data, and described at least one injecting data comprises at least one indirect instruction.
8. the satellite instruction sequence treating apparatus based on multitask according to claim 6, is characterized in that, described instruction sequence form is:
Length: start the total byte length finishing to assignment instructions list field for identifying from validity field;
Type: the different instruction task type of carrying out for distinguishing satellite;
Verification and: for identifying the cumulative sum verification that starts to finish to assignment instructions list field all bytes from validity field, only have verification just can carry out this instruction sequence via satellite;
Validity: custom feature;
Number of tasks: for identifying all instruction task quantity;
Total instruction number: for identifying the total instruction number comprising when time instruction sequence;
Mission bit stream: for identifying the corresponding initial order number information of all instruction tasks, every instruction task has two byte information;
Assignment instructions list: detailed for identifying all instructions.
9. the satellite instruction sequence treating apparatus based on multitask according to claim 6, is characterized in that, described number of tasks is from 1 open numbering.
10. the satellite instruction sequence treating apparatus based on multitask according to claim 6, is characterized in that, in described mission bit stream, the initial order of all instruction tasks numbering is from 1 open numbering, and the initial order of dummy instruction task numbering fixedly fills out 0.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410210694.1A CN103984592B (en) | 2014-05-19 | 2014-05-19 | A kind of satellite command series processing method and device based on multitask |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410210694.1A CN103984592B (en) | 2014-05-19 | 2014-05-19 | A kind of satellite command series processing method and device based on multitask |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103984592A true CN103984592A (en) | 2014-08-13 |
| CN103984592B CN103984592B (en) | 2017-07-11 |
Family
ID=51276584
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410210694.1A Expired - Fee Related CN103984592B (en) | 2014-05-19 | 2014-05-19 | A kind of satellite command series processing method and device based on multitask |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103984592B (en) |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105511311A (en) * | 2015-11-30 | 2016-04-20 | 上海卫星工程研究所 | High-efficiency remote-sensing satellite multi-system cooperation integration control method |
| CN105763643A (en) * | 2016-04-20 | 2016-07-13 | 航天东方红卫星有限公司 | Minisatellite electronic load task uploading method using task template |
| CN105959055A (en) * | 2016-04-15 | 2016-09-21 | 上海微小卫星工程中心 | Aerospace vehicle and telemetering method thereof |
| CN106406863A (en) * | 2016-08-31 | 2017-02-15 | 西安空间无线电技术研究所 | Security reconfiguration method of in-orbit data for manned aircraft instrument software |
| CN107506892A (en) * | 2017-07-17 | 2017-12-22 | 北京空间飞行器总体设计部 | It is a kind of towards the ground integrated Intelligent control system of quiet rail Optical remote satellite star |
| CN110034814A (en) * | 2019-03-29 | 2019-07-19 | 航天东方红卫星有限公司 | Quick satellite task triggers mode instruction design method |
| CN110398985A (en) * | 2019-08-14 | 2019-11-01 | 北京信成未来科技有限公司 | A kind of distributed self-adaption Telemetry System of UAV and method |
| CN112328209A (en) * | 2020-10-22 | 2021-02-05 | 中国科学院国家空间科学中心 | Editing and checking method for deep space probe payload data injection packet |
| CN112650198A (en) * | 2020-12-21 | 2021-04-13 | 中国人民解放军63920部队 | Multi-spacecraft injection plan automatic generation and control method and device |
| CN113110308A (en) * | 2021-02-25 | 2021-07-13 | 北京空间飞行器总体设计部 | Lunar surface sampling three-in-one flight control cooperative work flow optimization method |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20050030226A1 (en) * | 2003-08-05 | 2005-02-10 | Miyamoto Ryan Y. | Microwave self-phasing antenna arrays for secure data transmission & satellite network crosslinks |
| US20050094591A1 (en) * | 2003-11-05 | 2005-05-05 | Kwon Hyuk-Joon | Wireless remote controller using time division protocol and satellite radio receiver including the same |
| CN101145271A (en) * | 2007-10-30 | 2008-03-19 | 航天东方红卫星有限公司 | Satellite remote command operational method |
| CN101876699A (en) * | 2009-04-30 | 2010-11-03 | 中国科学院空间科学与应用研究中心 | Control system and control method of satellite-borne microwave radiometer |
| CN102081704A (en) * | 2011-01-25 | 2011-06-01 | 中国科学院国家天文台 | Generation method for ontrack-operation injection data of scientific detecting instrument lunar probe |
| CN102520715A (en) * | 2011-12-28 | 2012-06-27 | 北京航空航天大学 | Universal satellite ground overall control test system |
-
2014
- 2014-05-19 CN CN201410210694.1A patent/CN103984592B/en not_active Expired - Fee Related
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20050030226A1 (en) * | 2003-08-05 | 2005-02-10 | Miyamoto Ryan Y. | Microwave self-phasing antenna arrays for secure data transmission & satellite network crosslinks |
| US20050094591A1 (en) * | 2003-11-05 | 2005-05-05 | Kwon Hyuk-Joon | Wireless remote controller using time division protocol and satellite radio receiver including the same |
| CN101145271A (en) * | 2007-10-30 | 2008-03-19 | 航天东方红卫星有限公司 | Satellite remote command operational method |
| CN101876699A (en) * | 2009-04-30 | 2010-11-03 | 中国科学院空间科学与应用研究中心 | Control system and control method of satellite-borne microwave radiometer |
| CN102081704A (en) * | 2011-01-25 | 2011-06-01 | 中国科学院国家天文台 | Generation method for ontrack-operation injection data of scientific detecting instrument lunar probe |
| CN102520715A (en) * | 2011-12-28 | 2012-06-27 | 北京航空航天大学 | Universal satellite ground overall control test system |
Cited By (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105511311A (en) * | 2015-11-30 | 2016-04-20 | 上海卫星工程研究所 | High-efficiency remote-sensing satellite multi-system cooperation integration control method |
| CN105511311B (en) * | 2015-11-30 | 2018-05-18 | 上海卫星工程研究所 | Efficient remote sensing satellite multisystem coordination with the synthesis control method |
| CN105959055A (en) * | 2016-04-15 | 2016-09-21 | 上海微小卫星工程中心 | Aerospace vehicle and telemetering method thereof |
| CN105959055B (en) * | 2016-04-15 | 2019-07-12 | 上海微小卫星工程中心 | A kind of aerospace vehicle and its method of telemetering |
| CN105763643B (en) * | 2016-04-20 | 2018-12-21 | 航天东方红卫星有限公司 | Injecting method on a kind of moonlet electronics load task using task template |
| CN105763643A (en) * | 2016-04-20 | 2016-07-13 | 航天东方红卫星有限公司 | Minisatellite electronic load task uploading method using task template |
| CN106406863A (en) * | 2016-08-31 | 2017-02-15 | 西安空间无线电技术研究所 | Security reconfiguration method of in-orbit data for manned aircraft instrument software |
| CN106406863B (en) * | 2016-08-31 | 2019-07-12 | 西安空间无线电技术研究所 | A kind of in-orbit data safety method for reconfiguration for the instruments and meters software that carries people to fly |
| CN107506892A (en) * | 2017-07-17 | 2017-12-22 | 北京空间飞行器总体设计部 | It is a kind of towards the ground integrated Intelligent control system of quiet rail Optical remote satellite star |
| CN110034814A (en) * | 2019-03-29 | 2019-07-19 | 航天东方红卫星有限公司 | Quick satellite task triggers mode instruction design method |
| CN110034814B (en) * | 2019-03-29 | 2021-07-13 | 航天东方红卫星有限公司 | Agile satellite task trigger mode instruction design method |
| CN110398985A (en) * | 2019-08-14 | 2019-11-01 | 北京信成未来科技有限公司 | A kind of distributed self-adaption Telemetry System of UAV and method |
| CN112328209A (en) * | 2020-10-22 | 2021-02-05 | 中国科学院国家空间科学中心 | Editing and checking method for deep space probe payload data injection packet |
| CN112650198A (en) * | 2020-12-21 | 2021-04-13 | 中国人民解放军63920部队 | Multi-spacecraft injection plan automatic generation and control method and device |
| CN113110308A (en) * | 2021-02-25 | 2021-07-13 | 北京空间飞行器总体设计部 | Lunar surface sampling three-in-one flight control cooperative work flow optimization method |
Also Published As
| Publication number | Publication date |
|---|---|
| CN103984592B (en) | 2017-07-11 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN103984592A (en) | Satellite instruction sequence processing method and device based on multiple tasks | |
| CN104850132B (en) | A kind of multitask load management device and method | |
| CN112491457B (en) | Satellite on-orbit reconstruction method, device, system, equipment and storage medium | |
| CN102841846B (en) | A kind of method for testing software based on Hadoop, device and system | |
| CN105472083B (en) | The test method and system of wireless terminal | |
| CN104158627B (en) | A kind of automatic recognition system and method for heterogeneous links multi-protocols | |
| CN106020948A (en) | Flow process scheduling method and device | |
| CN101882089A (en) | Method for processing business conversational application with multi-thread and device thereof | |
| CN106445800A (en) | Chip verification method and device | |
| KR100911162B1 (en) | Satellite Mission Control Apparatus | |
| CN102664779A (en) | CAN bus data transmitting method | |
| CN109685499A (en) | A kind of SIM card and implementation method of embedded digital wallet function | |
| CN102622550A (en) | Safe online patch check system facing terminal computers | |
| CN109188471B (en) | Satellite fault diagnosis method based on software implementation | |
| CN105334756A (en) | Agile satellite mission interpretation closed loop simulation verification system and method | |
| KR20200080044A (en) | Command processing device in satellite and the controlling method thereof | |
| CN110035103A (en) | A kind of transferable distributed scheduling system of internodal data | |
| CN107370535A (en) | Incorporate based on microsatellite system timely responds to information acquisition method | |
| CN104267622A (en) | Satellite telemetering acquisition device and method based on tasks and time | |
| CN113190253B (en) | Software online upgrading system and method applied to onboard IMA | |
| CN103973581A (en) | Method, device and system for processing message data | |
| CN104753582B (en) | The ground validation system and its experimental method of spatial information quick response | |
| CN103116546A (en) | Automatic ground verification system for satellite on-orbit large-scale program modification | |
| CN107976703B (en) | Differential positioning optimization method and system, positioning terminal and memory | |
| CN106411675A (en) | Centralized bus timing control method based on time slice planning |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170711 Termination date: 20180519 |