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42results about How to "Improve mission performance" patented technology

Mobile edge network intelligent resource allocation method capable of dividing tasks

The invention relates to a mobile edge network intelligent resource allocation method capable of dividing tasks, which comprises the following steps of: dividing serial tasks generated by a terminal to obtain a plurality of subtasks, and establishing an unloading task model; respectively establishing a time delay model and an energy consumption model for the subtasks according to a local execution mode or an unloading execution mode, and defining an unloading joint target optimization function based on a multi-user serial dependent task; in a multi-server scene, establishing a Markov game model according to a cooperative competition relationship of multiple users to wireless communication and computing resources, and optimizing the unloading joint target optimization function; and in a time-varying environment, taking each terminal as an independent agent based on part of system state information to execute a reinforcement learning algorithm to solve the Markov game model, and determining an unloading strategy, sub-channel selection, transmitting power and resource allocation quantity. According to the mobile edge network intelligent resource allocation method, server resources can be reasonably allocated, fragmented resources can be fully used, the terminal user experience is ensured, and the network operation stability is improved.
Owner:SHANGHAI INST OF MICROSYSTEM & INFORMATION TECH CHINESE ACAD OF SCI

Attitude compensation method of agile satellite imagery in reverse push-broom mismatch

ActiveCN102229362ASolve task planning and scheduling problemsImprove mission performanceImage analysisSpacecraft guiding apparatusEarth's rotationBroom
The invention discloses an attitude compensation method of agile satellite imagery in reverse push-broom mismatch. Aiming at the defect (only considering the drift current effect brought by earth rotation) of the attitude compensation method in the traditional imagery mode (the satellite directing over the ground is fixed), through analyzing the generation reason of a drift angle under the imagery mode of constantly changing satellite reverse push-broom attitude directing over the ground (constantly changing attitude directing over the ground under the condition of mismatch between the substellar point speed and the camera push-broom speed), the drift current effect of imagery is considered from three aspects (orbital motion, earth rotation and camera push-broom speed), a drift current angle calculation formula under the mode is obtained according to the orbital attitude parameters combining the basic definition of the drift angle, on the basis, the satellite attitude compensation method is obtained by combining the basic principle of TDICCD (time delayed and integration charge coupled device) imagery and the yaw control principle, and the imagery requirement of agile satellite reverse push-broom can be satisfied.
Owner:AEROSPACE DONGFANGHONG SATELLITE

Edge computing task processing and scheduling method and device in industrial Internet environment

The invention discloses an edge computing task processing and scheduling method and device in an industrial Internet environment, and the device comprises the steps that an information feedback modulecollects periodic broadcast information of a base station associated with each set user equipment UE in a target region and transmits the periodic broadcast information to an information analysis andprocessing unit, a terminal equipment monitoring unit collects or receives the monitoring information of each UE and sends the monitoring information to the information analysis and processing unit,an information monitoring module collects real-time parameter data of each UE and sends the real-time parameter data to a heterogeneous data processing unit, a service priority processing unit and a terminal equipment monitoring unit, the information analysis and processing unit generates a state feedback result corresponding to the UE according to the received information and sends the state feedback result to the information feedback module and an equipment flow overall scheduling module, and a scheduling module generates an overall resource scheduling instruction according to the state feedback result and the feedback information of a task unloading decision unit, sends the overall resource scheduling instruction to each MEC through the information feedback module, and sends the condition information of the MEC to the task unloading decision unit.
Owner:COMP NETWORK INFORMATION CENT CHINESE ACADEMY OF SCI

Attitude Compensation Method for Agile Satellite Imaging with Pushbroom Velocity Mismatch in Any Direction

The invention relates to a posture compensation method for dealing with mismatching of a push-scanning speed for imaging along random direction of a quick satellite. For breaking through the limitation (only taking the deflecting effect caused by earth rotation into consideration) of the posture compensation method under a traditional imaging mode (fixed direction from satellite to earth), the reason why the deflecting effect is generated under the imaging mode with constantly changing posture-to-earth direction (namely, posture-to-earth direction constantly changes under the condition of mismatching between a satellite spot speed and a camera push-scanning speed) when the satellite is used for push-scanning along random direction is analyzed and the imaging deflecting effect is analyzed from three aspects of orbital motion, earth rotation and camera push-scanning speed, thereby acquiring a deflecting angle calculation formula under such a mode according to the track posture parameters and the basic definition of a deflecting angle. Based on the deflecting angle calculation formula and a basic principle of TDICCD (Time Delay Integral Charge-coupled Device) imaging as well as a yawcontrol principle, the posture compensation method, which can meet the imaging requirement for push-scanning along random direction of the quick satellite, is provided.
Owner:AEROSPACE DONGFANGHONG SATELLITE

On-orbit assembly spacecraft based on pre-integrated truss

InactiveCN110182388AOvercome the lack of launch capabilityMeet the needs of in-orbit applicationsCosmonautic vehiclesCosmonautic partsChinese charactersComputer module
The invention discloses an on-orbit assembly spacecraft based on a pre-integrated truss, and relates to the technical field of spacecraft on-orbit service. The on-orbit assembly spacecraft comprises apre-integrated truss structure, four solar battery arrays, a storage battery pack, two propelling modules, a pose measurement and control module and a digital management module; the pre-integrated truss structure is of a support structure with a Chinese character "jing" shape which is formed by four supports; the four solar battery arrays are symmetrically installed at the two ends of two opposite supports of the pre-integrated truss structure; the storage battery pack is installed on the outer side wall of one support of the pre-integrated truss structure; the pose measurement and controlling module is installed on the outer side wall of the support, which is opposite to the storage battery pack, of the pre-integrated truss structure; the two propelling modules are symmetrically installed on the outer side walls of the other two opposite supports of the pre-integrated truss structure; and the digital management module is installed on the inner side wall of one support of the pre-integrated truss structure. The on-orbit assembly spacecraft provides a novel means for on-orbit application of a large spacecraft, and can implement tasks such as on-orbit assembly and on-orbit functionexpansion.
Owner:CHINA ACADEMY OF SPACE TECHNOLOGY

Attitude Compensation Method for Agile Satellite Imaging Side Swing Pushbroom Velocity Mismatch

The invention discloses a posture compensation method in case of mismatched side-swing push-broom velocity in imaging of an agile satellite. For the limitation (only the drift action caused by auto-rotation of the earth is considered) of the posture compensation method in the traditional imaging mode (the pointing direction of the satellite to the ground is fixed), the drift angle calculation formula is obtained under the mode according to the track posture parameter by analyzing the reason for the generation of the drift angle under the imaging mode (namely the condition that the substellar point velocity is mismatched with the push-broom velocity of a camera, and the pointing direction of the posture at the moment to the earth changes continuously) that the pointing direction of the side-swing push-broom posture of the satellite to the earth changes continuously, considering the drift action of the imaging from the three aspects such as orbital motion, auto-rotation of the earth andthe push-broom velocity of a camera and combining the basic definition of the drift angle. On the basis, by combination of the basic principle of TDICCD (time delay integration charged coupling device) imaging and the yawing control principle, the satellite posture compensation method is given, so that the imaging requirement for side-swing push and broom of the agile satellite can be met.
Owner:AEROSPACE DONGFANGHONG SATELLITE

Task migration method and system of underwater ad hoc network based on edge gateway

The invention discloses a task migration method and system of an underwater ad hoc network based on an edge gateway. The method comprises the steps of selecting the edge gateway used for task migration management; adding sensor node information to a resource manager of the edge gateway; arranging the sensor node information by the edge gateway to form priority ranking of the nodes in the resourcequeue; arranging the task information of the original sensor nodes in a descending order by the edge gateway according to task priorities and puts the task information into a task queue of a task manager, and selecting an optimal task cooperation node; and migrating the task to the task cooperation node through the edge gateway for task calculation, and sending a calculation result to the originalsensor node. According to the method, the underwater self-organizing network node sends the collected seabed heterogeneous data to the nearest edge gateway, and the edge gateway migrates the task ofthe resource-limited node to the node with rich resources for cooperative completion, thereby balancing the network load, reducing the node energy consumption, and improving the marine data observation efficiency.
Owner:OCEANOGRAPHIC INSTR RES INST SHANDONG ACAD OF SCI

Multi-target positioning method based on single aircraft seeker image information

The invention belongs to the technical field of aircrafts, and provides a method for positioning multiple targets according to image information of a single aircraft seeker. The method comprises the steps: based on seeker image information, providing a multi-target positioning method under two conditions that the reference target position is known and unknown; if the position of the reference target is known, measuring the relative orientation, perpendicular to the sight line, of the multiple targets and the reference target through seeker image information and converting the relative orientation into a ground coordinate system, so if the position of the reference target is known, the position of the auxiliary point can be obtained; extending the connecting line of the aircraft and the auxiliary point to the ground to obtain a multi-target position estimation value; if the position of the reference target is unknown, measuring the orientation of multiple targets by using seeker image information to obtain the unit relative position vector of the aircraft and the multiple targets, converting the unit relative position vector to a ground coordinate system, and enabling the relative position vector of the aircraft and the targets to be extended to the ground to obtain a target position estimated value. The method can be applied to ground target tasks of various aircrafts, and the environment adaptive capacity and the task execution capacity are improved.
Owner:NAT INNOVATION INST OF DEFENSE TECH PLA ACAD OF MILITARY SCI

Reduce task execution method and device in Spark framework, equipment and storage medium

The invention discloses a Reduce task execution method and device in a Spark framework, equipment and a storage medium, and the method comprises the steps: obtaining a first number of Executors required for executing a Reduce task of an application program, and determining a second number of available Executors in a Spark framework node; determining the first number of the available Executors from the second number of the available Executors on the basis of the communication distance between the available Executors, so as to obtain a target Executor set which is corresponding to the application program and has low communication delay; wherein the communication distance represents the communication delay between the nodes where the available Executors are located; and the available Executor in the target Executor set is started in a corresponding Spark framework node, so that the Reduce task of the application program is executed by utilizing the started available Executor. It can be seen that the Executors are started on the nodes close to each other in the Spark framework by taking the communication distance as a main consideration factor, so that communication delay between Reduce tasks during operation running is reduced, and task execution performance is improved.
Owner:NANHUA UNIV

Posture compensation method in case of mismatched side-swing push-broom velocity in imaging of agile satellite

The invention discloses a posture compensation method in case of mismatched side-swing push-broom velocity in imaging of an agile satellite. For the limitation (only the drift action caused by auto-rotation of the earth is considered) of the posture compensation method in the traditional imaging mode (the pointing direction of the satellite to the ground is fixed), the drift angle calculation formula is obtained under the mode according to the track posture parameter by analyzing the reason for the generation of the drift angle under the imaging mode (namely the condition that the substellar point velocity is mismatched with the push-broom velocity of a camera, and the pointing direction of the posture at the moment to the earth changes continuously) that the pointing direction of the side-swing push-broom posture of the satellite to the earth changes continuously, considering the drift action of the imaging from the three aspects such as orbital motion, auto-rotation of the earth andthe push-broom velocity of a camera and combining the basic definition of the drift angle. On the basis, by combination of the basic principle of TDICCD (time delay integration charged coupling device) imaging and the yawing control principle, the satellite posture compensation method is given, so that the imaging requirement for side-swing push and broom of the agile satellite can be met.
Owner:AEROSPACE DONGFANGHONG SATELLITE
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