CN112991512A - Rapid scene model construction method based on measurement and control task analysis system model base - Google Patents
Rapid scene model construction method based on measurement and control task analysis system model base Download PDFInfo
- Publication number
- CN112991512A CN112991512A CN202110170611.0A CN202110170611A CN112991512A CN 112991512 A CN112991512 A CN 112991512A CN 202110170611 A CN202110170611 A CN 202110170611A CN 112991512 A CN112991512 A CN 112991512A
- Authority
- CN
- China
- Prior art keywords
- model
- scene
- measurement
- control
- request
- 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.)
- Withdrawn
Links
- 238000005259 measurement Methods 0.000 title claims abstract description 65
- 238000010276 construction Methods 0.000 title claims abstract description 7
- 238000003780 insertion Methods 0.000 claims abstract description 22
- 230000037431 insertion Effects 0.000 claims abstract description 22
- 238000000034 method Methods 0.000 claims abstract description 18
- 238000013507 mapping Methods 0.000 claims abstract description 4
- 230000004044 response Effects 0.000 claims description 18
- 239000007787 solid Substances 0.000 claims description 9
- 230000005540 biological transmission Effects 0.000 claims description 7
- 238000011084 recovery Methods 0.000 claims description 7
- 239000002775 capsule Substances 0.000 claims description 6
- 238000012216 screening Methods 0.000 claims description 6
- 238000013461 design Methods 0.000 claims description 3
- 238000005728 strengthening Methods 0.000 abstract description 2
- 238000010586 diagram Methods 0.000 description 3
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000008569 process Effects 0.000 description 2
Images
Classifications
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06T—IMAGE DATA PROCESSING OR GENERATION, IN GENERAL
- G06T17/00—Three dimensional [3D] modelling, e.g. data description of 3D objects
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F16/00—Information retrieval; Database structures therefor; File system structures therefor
- G06F16/20—Information retrieval; Database structures therefor; File system structures therefor of structured data, e.g. relational data
- G06F16/25—Integrating or interfacing systems involving database management systems
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Theoretical Computer Science (AREA)
- General Physics & Mathematics (AREA)
- Databases & Information Systems (AREA)
- Computer Graphics (AREA)
- Geometry (AREA)
- Software Systems (AREA)
- Data Mining & Analysis (AREA)
- General Engineering & Computer Science (AREA)
- Radar Systems Or Details Thereof (AREA)
Abstract
The invention belongs to the technical field of spacecraft flight measurement and control, and particularly relates to a rapid scene model construction method based on a measurement and control task analysis system model base. The method comprises the following steps: the method comprises the steps of establishing a model database, establishing a mapping relation between the model database and the model database, establishing an access relation of a space flight measurement and control system, a user and a scene to the model database, storing an external input request, analyzing and feeding back an external output request, analyzing an external insertion request and inserting a model into the scene. Compared with the prior art, the invention provides a method for realizing the rapid construction of the measurement and control scene model in consideration of strengthening the universality of the model, avoiding the repeated work and improving the work efficiency according to the measurement and control task requirements, can use the functions of the model library, can be rapidly inserted into the existing model in the model library when the task scene is created, strengthens the universality of the model, avoids the repeated work and improves the work efficiency.
Description
Technical Field
The invention belongs to the technical field of spacecraft flight measurement and control, and particularly relates to a rapid scene model construction method based on a measurement and control task analysis system model base.
Background
When a transmission task measurement and control scheme is designed in a measurement and control task analysis system, a scene needs to be created according to task requirements. The creation of a complete measurement and control task scene requires the addition of various models mounted under ballistic devices, track devices, measurement and control station devices and landing recovery devices and the setting of the attributes thereof, which is very complicated. Every time a scene is created, a large number of models need to be added and model attributes need to be set, and the types and attributes of the models required by each measurement and control task have certain universality and similarity.
Disclosure of Invention
Technical problem to be solved
The technical problem to be solved by the invention is as follows: according to the measurement and control task requirements, a multi-target measurement and control scene model is quickly constructed in the measurement and control task analysis system.
(II) technical scheme
In order to solve the technical problems, the invention provides a method for quickly constructing a scene model based on a measurement and control task analysis system model library, which comprises the following steps:
step S1: when the space flight measurement and control system carries out the design of a launching task measurement and control scheme, a user firstly creates a task scene according to task requirements; a user is a transmitting task measurement and control scheme designer; the task scene is a set of ballistic equipment, track equipment, measurement and control station equipment and landing recovery equipment required by the task; according to the requirements of the measurement and control tasks, a model database comprising ballistic equipment, track equipment, measurement and control station equipment and landing equipment is established in each scene; each model stored in the model database is a model item, and each model item comprises two three-dimensional models and attributes;
step S2: establishing a mapping relation between the model database and the model database according to the model items in the model database, and taking the names of the model items as connecting keys of the model database and the model database;
the model database is used as a connecting link between a task scene and the model database, and can be connected to relevant data for calling the model item in the model database through the name of the model item in the model database;
step S3: establishing an access relation of the space flight measurement and control system, the user and the scene to the model base according to the authority relation of the space flight measurement and control system, the user and the task scene; the access relation determines that each user in the aerospace measurement and control system can only access the model base of the user, and all task scenes created by the user can access the model base corresponding to the user; the access mode is realized by an external input request, an external input request and an external insertion request from a user;
step S4: analyzing the type category of the model contained in the external input request according to the external input request, then dividing the model contained in the external input request according to the type of the model, storing the model into a model item to which the type of the model belongs in a model library, and binding the name of the stored model with a scene; the naming and scene binding of the model means: the model name comprises a scene name;
if the model contained in the external input request is the entity model, the mounted additional models thereof and attribute information of all models are stored;
if the model contained in the external input request is the additional model, independently storing the additional model and the attribute information thereof;
in order to distinguish the same type of models in the model library, the entity model naming format is 'scene name-entity model name', and the additional model naming format is 'scene name-entity model name-additional model name', so that a user can browse the stored models in the model library conveniently;
step S5: judging the model type required by the external output request according to the external output request, and feeding back request response data; the request response data is all model names which are the same as the model types required by the external output request;
when an external output request is received, searching all models with the same type according to the model type required by the external output request, and taking all model names as request response data;
step S6: according to the request response data of step S5, the user issues an external insertion request again, the external insertion request including one or more model names; wherein the one or more model names are names of one or more models of all models of the same type in the request response data;
and then calling data of the corresponding model from the model database according to the model name in the external insertion request, and inserting the data of the corresponding model into the scene.
Wherein, the steps S5 and S6 function similarly to the primary screening and fine screening processes, step S5 searches all model names containing fuzzy keywords, which may be attributed to different model items, i.e. for different devices, and all searched model names are fed back to the user by means of requesting response data, and then the user inserts a request through the outside of step S6, thereby specifying exactly which models are needed for call insertion.
In step S1, for the model item corresponding to the ballistic device, the two-dimensional model includes: the system comprises a physical model rocket, a returning capsule and an additional model mounted on the physical model rocket, the returning capsule and the additional model, wherein the additional model comprises a security control receiver, a security control transmitter, a remote measuring receiver, a remote measuring transmitter and a pulse radar.
In step S1, the two-dimensional model of the model item of the corresponding track device includes: the system comprises a solid model detector, a relay satellite and an additional model mounted by the relay satellite.
In step S1, for the model item corresponding to the measurement and control station device, the two-dimensional model includes: the system comprises a solid model transmitting station, a measurement and control station, a measuring ship and an additional model for mounting the measuring ship.
In step S1, the two-dimensional model of the model item corresponding to the landing recovery device includes: solid model ground vehicles, airplanes, helicopter models.
Wherein, in the step S1, each model includes different attributes, including: basic attribute, two-three-dimensional attribute, constraint attribute and radio frequency environment attribute.
In step S1, each attribute includes a plurality of attribute elements; wherein,
the basic attributes of the entity model rocket comprise a plurality of attribute elements including orbit starting time, orbit ending time, orbit ephemeris and orbit attitude;
the basic attribute of the security control transmitter as an additional model comprises a plurality of attribute elements including uplink frequency, transmission power and transmission antenna gain.
In step S3, each user may create a personal model library for the user, which is applied to different scenes and between scenes constructed by the user.
In step S6, if the model name in the external insertion request corresponds to the entity model, the entity model and the attached model thereof are inserted, and the attribute information of the model is saved;
and if the model name in the external insertion request corresponds to the additional model, only the additional model and the attribute information thereof are inserted.
(III) advantageous effects
Compared with the prior art, the invention provides a method for realizing the rapid construction of the measurement and control scene model in consideration of strengthening the universality of the model, avoiding the repeated work and improving the work efficiency according to the measurement and control task requirements, can use the functions of the model library, can be rapidly inserted into the existing model in the model library when the task scene is created, strengthens the universality of the model, avoids the repeated work and improves the work efficiency.
Drawings
Fig. 1 is a diagram of a rights relationship structure.
FIG. 2 is a functional explanatory diagram of a measurement and control task analysis system model library.
Detailed Description
In order to make the objects, contents, and advantages of the present invention clearer, the following detailed description of the embodiments of the present invention will be made in conjunction with the accompanying drawings and examples.
In order to solve the problems in the prior art, the invention provides a method for quickly constructing a scene model based on a measurement and control task analysis system model base, which comprises the following steps of:
step S1: when the space flight measurement and control system carries out the design of a launching task measurement and control scheme, a user firstly creates a task scene according to task requirements; a user is a transmitting task measurement and control scheme designer; the task scene is a set of ballistic equipment, track equipment, measurement and control station equipment and landing recovery equipment required by the task; according to the requirements of the measurement and control tasks, a model database comprising ballistic equipment, track equipment, measurement and control station equipment and landing equipment is established in each scene; each model stored in the model database is a model item, and each model item comprises two three-dimensional models and attributes;
step S2: establishing a mapping relation between the model database and the model database according to the model items in the model database, and taking the names of the model items as connecting keys of the model database and the model database;
the model database is used as a connecting link between a task scene and the model database, and can be connected to relevant data for calling the model item in the model database through the name of the model item in the model database;
step S3: establishing an access relation of the space flight measurement and control system, the user and the scene to the model base according to the authority relation of the space flight measurement and control system, the user and the task scene; the access relation determines that each user in the aerospace measurement and control system can only access the model base of the user, and all task scenes created by the user can access the model base corresponding to the user; the access mode is realized by an external input request, an external input request and an external insertion request from a user;
step S4: analyzing the type category of the model contained in the external input request according to the external input request, then dividing the model contained in the external input request according to the type of the model, storing the model into a model item to which the type of the model belongs in a model library, and binding the name of the stored model with a scene; the naming and scene binding of the model means: the model name comprises a scene name;
if the model contained in the external input request is the entity model, the mounted additional models thereof and attribute information of all models are stored;
if the model contained in the external input request is the additional model, independently storing the additional model and the attribute information thereof;
in order to distinguish the same type of models in the model library, the entity model naming format is 'scene name-entity model name', and the additional model naming format is 'scene name-entity model name-additional model name', so that a user can browse the stored models in the model library conveniently;
step S5: judging the model type required by the external output request according to the external output request, and feeding back request response data; the request response data is all model names which are the same as the model types required by the external output request;
when an external output request is received, searching all models with the same type according to the model type required by the external output request, and taking all model names as request response data;
step S6: according to the request response data of step S5, the user issues an external insertion request again, the external insertion request including one or more model names; wherein the one or more model names are names of one or more models of all models of the same type in the request response data;
and then calling data of the corresponding model from the model database according to the model name in the external insertion request, and inserting the data of the corresponding model into the scene.
Wherein, the steps S5 and S6 function similarly to the primary screening and fine screening processes, step S5 searches all model names containing fuzzy keywords, which may be attributed to different model items, i.e. for different devices, and all searched model names are fed back to the user by means of requesting response data, and then the user inserts a request through the outside of step S6, thereby specifying exactly which models are needed for call insertion.
In step S1, for the model item corresponding to the ballistic device, the two-dimensional model includes: the system comprises a physical model rocket, a returning capsule and an additional model mounted on the physical model rocket, the returning capsule and the additional model, wherein the additional model comprises a security control receiver, a security control transmitter, a remote measuring receiver, a remote measuring transmitter and a pulse radar.
In step S1, the two-dimensional model of the model item of the corresponding track device includes: the system comprises a solid model detector, a relay satellite and an additional model mounted by the relay satellite.
In step S1, for the model item corresponding to the measurement and control station device, the two-dimensional model includes: the system comprises a solid model transmitting station, a measurement and control station, a measuring ship and an additional model for mounting the measuring ship.
In step S1, the two-dimensional model of the model item corresponding to the landing recovery device includes: solid model ground vehicles, airplanes, helicopter models.
Wherein, in the step S1, each model includes different attributes, including: basic attribute, two-three-dimensional attribute, constraint attribute and radio frequency environment attribute.
In step S1, each attribute includes a plurality of attribute elements; wherein,
the basic attributes of the entity model rocket comprise a plurality of attribute elements including orbit starting time, orbit ending time, orbit ephemeris and orbit attitude;
the basic attribute of the security control transmitter as an additional model comprises a plurality of attribute elements including uplink frequency, transmission power and transmission antenna gain.
In step S3, as can be seen from the authority relationship structure diagram 1, each user may create a personal model library of the user, and apply the model library to different scenes and between scenes constructed by the user.
In step S6, if the model name in the external insertion request corresponds to the entity model, the entity model and the attached model thereof are inserted, and the attribute information of the model is saved.
In step S6, if the model name in the external insertion request corresponds to the additional model, only the additional model and its attribute information are inserted.
The above description is only a preferred embodiment of the present invention, and it should be noted that, for those skilled in the art, several modifications and variations can be made without departing from the technical principle of the present invention, and these modifications and variations should also be regarded as the protection scope of the present invention.
Claims (10)
1. A method for quickly constructing a scene model based on a measurement and control task analysis system model base is characterized by comprising the following steps:
step S1: when the space flight measurement and control system carries out the design of a launching task measurement and control scheme, a user firstly creates a task scene according to task requirements; a user is a transmitting task measurement and control scheme designer; the task scene is a set of ballistic equipment, track equipment, measurement and control station equipment and landing recovery equipment required by the task; according to the requirements of the measurement and control tasks, a model database comprising ballistic equipment, track equipment, measurement and control station equipment and landing equipment is established in each scene; each model stored in the model database is a model item, and each model item comprises two three-dimensional models and attributes;
step S2: establishing a mapping relation between the model database and the model database according to the model items in the model database, and taking the names of the model items as connecting keys of the model database and the model database;
the model database is used as a connecting link between a task scene and the model database, and can be connected to relevant data for calling the model item in the model database through the name of the model item in the model database;
step S3: establishing an access relation of the space flight measurement and control system, the user and the scene to the model base according to the authority relation of the space flight measurement and control system, the user and the task scene; the access relation determines that each user in the aerospace measurement and control system can only access the model base of the user, and all task scenes created by the user can access the model base corresponding to the user; the access mode is realized by an external input request, an external input request and an external insertion request from a user;
step S4: analyzing the type category of the model contained in the external input request according to the external input request, then dividing the model contained in the external input request according to the type of the model, storing the model into a model item to which the type of the model belongs in a model library, and binding the name of the stored model with a scene; the naming and scene binding of the model means: the model name comprises a scene name;
if the model contained in the external input request is the entity model, the mounted additional models thereof and attribute information of all models are stored;
if the model contained in the external input request is the additional model, independently storing the additional model and the attribute information thereof;
in order to distinguish the same type of models in the model library, the entity model naming format is 'scene name-entity model name', and the additional model naming format is 'scene name-entity model name-additional model name', so that a user can browse the stored models in the model library conveniently;
step S5: judging the model type required by the external output request according to the external output request, and feeding back request response data; the request response data is all model names which are the same as the model types required by the external output request;
when an external output request is received, searching all models with the same type according to the model type required by the external output request, and taking all model names as request response data;
step S6: according to the request response data of step S5, the user issues an external insertion request again, the external insertion request including one or more model names; wherein the one or more model names are names of one or more models of all models of the same type in the request response data;
and then calling data of the corresponding model from the model database according to the model name in the external insertion request, and inserting the data of the corresponding model into the scene.
2. The method for rapidly building the scene model based on the measurement and control task analysis system model library according to claim 1, wherein the steps S5 and S6 are similar to the primary screening and the fine screening, step S5 searches all model names containing fuzzy keywords, which may be attributed to different model items, i.e. used in different devices, all the searched model names are fed back to the user by means of requesting response data, and then the user inserts a request through the outside of step S6, thereby precisely specifying which models are specifically needed for call insertion.
3. The method for rapidly constructing a scene model based on a measurement and control task analysis system model library according to claim 1, wherein in step S1, for the model item corresponding to the ballistic device, the two-dimensional model includes: the system comprises a physical model rocket, a returning capsule and an additional model mounted on the physical model rocket, the returning capsule and the additional model, wherein the additional model comprises a security control receiver, a security control transmitter, a remote measuring receiver, a remote measuring transmitter and a pulse radar.
4. The method for rapidly building a scene model based on a measurement and control task analysis system model library according to claim 1, wherein in step S1, for the model item corresponding to the track device, the two-dimensional model includes: the system comprises a solid model detector, a relay satellite and an additional model mounted by the relay satellite.
5. The method for rapidly building a scene model based on a measurement and control task analysis system model library according to claim 1, wherein in step S1, for the model item corresponding to the measurement and control station device, the two-dimensional and three-dimensional models thereof include: the system comprises a solid model transmitting station, a measurement and control station, a measuring ship and an additional model for mounting the measuring ship.
6. The method for rapidly building a scene model based on a measurement and control task analysis system model library according to claim 1, wherein in step S1, for the model item corresponding to the landing recovery device, the two-dimensional model includes: solid model ground vehicles, airplanes, helicopter models.
7. The method for rapidly building a scene model based on a measurement and control task analysis system model library according to claim 1, wherein in the step S1, each model includes different attributes, including: basic attribute, two-three-dimensional attribute, constraint attribute and radio frequency environment attribute.
8. The method for rapidly building a scene model based on a measurement and control task analysis system model library according to claim 7, wherein in the step S1, each attribute further includes a plurality of attribute elements; wherein,
the basic attributes of the entity model rocket comprise a plurality of attribute elements including orbit starting time, orbit ending time, orbit ephemeris and orbit attitude;
the basic attribute of the security control transmitter as an additional model comprises a plurality of attribute elements including uplink frequency, transmission power and transmission antenna gain.
9. The method for rapid construction of scene models based on measurement and control task analysis system model library according to claim 1, wherein in step S3, each user can create the own personal model library for application in and between different scenes constructed by the user.
10. The method for rapidly building a scene model based on a measurement and control task analysis system model library according to claim 1, wherein in step S6, if the model name in the external insertion request corresponds to an entity model, the entity model and an attached model mounted thereon are inserted, and attribute information of the model is saved;
and if the model name in the external insertion request corresponds to the additional model, only the additional model and the attribute information thereof are inserted.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110170611.0A CN112991512A (en) | 2021-02-08 | 2021-02-08 | Rapid scene model construction method based on measurement and control task analysis system model base |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110170611.0A CN112991512A (en) | 2021-02-08 | 2021-02-08 | Rapid scene model construction method based on measurement and control task analysis system model base |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN112991512A true CN112991512A (en) | 2021-06-18 |
Family
ID=76349196
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202110170611.0A Withdrawn CN112991512A (en) | 2021-02-08 | 2021-02-08 | Rapid scene model construction method based on measurement and control task analysis system model base |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN112991512A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112991513A (en) * | 2021-02-08 | 2021-06-18 | 北京京航计算通讯研究所 | Rapid scene model construction system based on measurement and control task analysis system model base |
| CN116501650A (en) * | 2023-06-27 | 2023-07-28 | 航天科工火箭技术有限公司 | Method, device and medium for executing carrier rocket measurement and control flow engine |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20130082983A (en) * | 2011-12-26 | 2013-07-22 | (주)트라이디커뮤니케이션 | System for making contents and method thereof |
| CN104183023A (en) * | 2014-07-25 | 2014-12-03 | 天津多微信息技术有限公司 | Multi-scene graph construction method in distributed virtual environment |
| EP2993613A1 (en) * | 2014-09-04 | 2016-03-09 | Fujitsu Limited | A capture system arranged to create a 3d model from a scanned scene, a method and a graphical user interface |
| DE102017126389A1 (en) * | 2017-11-10 | 2019-05-16 | Liebherr-Werk Biberach Gmbh | Method and device for providing a workpiece representation at a production location |
| CN111666355A (en) * | 2020-06-12 | 2020-09-15 | 远光软件股份有限公司 | Model construction method and device for three-layer model of field, data and scene |
| CN111898007A (en) * | 2020-08-04 | 2020-11-06 | 广东电网有限责任公司电力科学研究院 | Three-dimensional scene model construction system and method for transformer substation |
| CN112991513A (en) * | 2021-02-08 | 2021-06-18 | 北京京航计算通讯研究所 | Rapid scene model construction system based on measurement and control task analysis system model base |
-
2021
- 2021-02-08 CN CN202110170611.0A patent/CN112991512A/en not_active Withdrawn
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20130082983A (en) * | 2011-12-26 | 2013-07-22 | (주)트라이디커뮤니케이션 | System for making contents and method thereof |
| CN104183023A (en) * | 2014-07-25 | 2014-12-03 | 天津多微信息技术有限公司 | Multi-scene graph construction method in distributed virtual environment |
| EP2993613A1 (en) * | 2014-09-04 | 2016-03-09 | Fujitsu Limited | A capture system arranged to create a 3d model from a scanned scene, a method and a graphical user interface |
| DE102017126389A1 (en) * | 2017-11-10 | 2019-05-16 | Liebherr-Werk Biberach Gmbh | Method and device for providing a workpiece representation at a production location |
| CN111666355A (en) * | 2020-06-12 | 2020-09-15 | 远光软件股份有限公司 | Model construction method and device for three-layer model of field, data and scene |
| CN111898007A (en) * | 2020-08-04 | 2020-11-06 | 广东电网有限责任公司电力科学研究院 | Three-dimensional scene model construction system and method for transformer substation |
| CN112991513A (en) * | 2021-02-08 | 2021-06-18 | 北京京航计算通讯研究所 | Rapid scene model construction system based on measurement and control task analysis system model base |
Non-Patent Citations (2)
| Title |
|---|
| HAN WANG ET AL.: "A Configurable Visual Steering Architecture based on 3D Scene Composition", 《PROCEEDINGS OF THE 2013 IEEE 17TH INTERNATIONAL CONFERENCE ON COMPUTER SUPPORTED COOPERATIVE WORK IN DESIGN (CSCWD)》 * |
| 谢晓方等: "基于三维模型库的战场想定配置软件", 《计算机与数字工程》 * |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112991513A (en) * | 2021-02-08 | 2021-06-18 | 北京京航计算通讯研究所 | Rapid scene model construction system based on measurement and control task analysis system model base |
| CN112991513B (en) * | 2021-02-08 | 2022-11-22 | 北京京航计算通讯研究所 | Rapid scene model construction system based on measurement and control task analysis system model base |
| CN116501650A (en) * | 2023-06-27 | 2023-07-28 | 航天科工火箭技术有限公司 | Method, device and medium for executing carrier rocket measurement and control flow engine |
| CN116501650B (en) * | 2023-06-27 | 2023-09-12 | 航天科工火箭技术有限公司 | Method, device and medium for executing carrier rocket measurement and control flow engine |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN112991512A (en) | Rapid scene model construction method based on measurement and control task analysis system model base | |
| US20210376918A1 (en) | Satellite control method and apparatus | |
| CN103954984A (en) | Personnel and transport vehicle positioning method for grain depot | |
| CN112991513B (en) | Rapid scene model construction system based on measurement and control task analysis system model base | |
| US10366183B2 (en) | System for modeling intelligent sensor selection and placement | |
| CN112835868A (en) | Method for constructing space frequency track resource comprehensive database | |
| US20060181403A1 (en) | Dynamically tasking one or more surveillance resources | |
| Nguyen | Future satellite system architectures and practical design issues: An overview | |
| Baceski et al. | HAVELSAT: A software defined radio experimentation CubeSat | |
| KR102436523B1 (en) | Integrated operator interface system and method for unmanned complex system | |
| Gaebler et al. | Identity management of clustered satellites with a generalized labeled multi-Bernoulli filter | |
| US20060173656A1 (en) | Dynamically tasking one or more surveillance resources | |
| Kurtulus et al. | ITU-pSAT I: Istanbul Technical University student pico-satellite program | |
| US7417538B2 (en) | Dynamically tasking one or more surveillance resources | |
| Rahayu et al. | Development of ground station performance information system for LAPAN satellite operations | |
| US10572563B2 (en) | Mobile computing systems and methods for accessing data | |
| CA3124968A1 (en) | Dynamic operation of satellite terminal | |
| US7408457B2 (en) | Dynamically tasking one or more surveillance resources | |
| Conto et al. | Use of SysML and model-based system engineering in the development of the Brazilian satellite VCUB1 | |
| CN116192222B (en) | Resource scheduling method and device for antenna array demand and computer equipment | |
| Kurniawan et al. | Software design to search data images of satellites LAPAN-A2/Orari and LAPAN-A3/IPB | |
| AU2022313102A1 (en) | Integrated platform for nanosatellite system data processing | |
| Wei et al. | Toolchain based hybrid implementation for GPS satellite communications with optical crosslinks | |
| Khulal et al. | Fabrication and Database Management of Cubesat | |
| JP2024527856A (en) | Integrated platform for nanosatellite system data processing |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20210618 |