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48 results about "Satellite scheduling" patented technology

Global positioning system satellite searching and scheduling method

The invention relates to the field of global satellite positioning and navigation, in particular to a satellite searching and dispatching method for a global positioning system (GPS); the method comprises three parts: a classifying satellite possibility dispatching method which comprises the steps as follows: the state of the satellite is judged by the obtained satellite information; each satellite is classified by the satellite state, thus presuming the searching scene further; according to the satellite classes and the searching scenes, different searching weights are arranged for each satellite so as to carry out the searching; a maintaining re-catching method for continuously searching the blocked satellites and a self-adaptive sensitiveness catching method which uses the catching methods of different sensitiveness by aiming at the satellites of different signal-noise-ratio. When the three methods are smartly used, the successful possibility of searching satellite is greatly improved, the time used for searching the satellite is reduced, the starting and positioning speed and the re-catching positioning precision are greatly improved, the power dissipation is reduced, and the problems of robustness and reliability in the satellite dispatching arithmetic are solved, thus improving the feasibility of the receiving machines in the urban forests where the blocking is severe, and greatly improving the experience of the user.
Owner:北京中科微知识产权服务有限公司

Agile satellite scheduling method considering time-dependent conversion time

The invention discloses an agile satellite scheduling method considering time-dependent conversion time. The agile satellite scheduling method comprises the steps of obtaining a to-be-observed targetsequence and preprocessing the to-be-observed target sequence; constructing an agile satellite scheduling model of time-dependent conversion time; inputting the preprocessed to-be-observed target sequence into an agile satellite scheduling model, and solving the agile satellite scheduling model; and outputting a solving result in the step 3 to obtain a scheduling scheme of the agile satellite. Dueto the fact that the time dependence of the attitude conversion time between the continuous observation tasks is considered, the constructed agile satellite scheduling model can better meet the scheduling requirement, and the scheduling efficiency of the solved scheduling scheme is higher. In the solving process, the earliest and latest unreachable time of each time window and the earliest starting time and latest starting time between any pair of observation windows in the same circle are pre-calculated, so that repeated calculation is reduced when insertion operation is tried, the calculation time is shortened, and the scheduling efficiency is improved.
Owner:NAT UNIV OF DEFENSE TECH

Relay satellite single-address antenna dynamic scheduling method for temporary task arrival

The invention belongs to the satellite scheduling field and relates to a relay satellite single-address antenna dynamic scheduling method for temporary task arrival. The method comprises the followingsteps: (1) according to the temporary task application information to be processed, matching the visible time window and the antenna available time window; if there are available time period resources, scheduling the temporary task; otherwise, proceeding to the next step; (2) analyzing the scheduled tasks that conflict with the temporary task requirements, and generating t set of tasks to be adjusted at the current layer; (3) trying to adjust the tasks to be adjusted, and if the scheduling is successful, putting an end to the scheduling process; otherwise proceeding to the next step; 4) deleting the resources occupied by the tasks to be adjusted in the current layer, and after scheduling the original temporary tasks, treating the tasks to be adjusted in the current layer as new temporarytasks respectively, so as to realize the expansion operation of the adjustment tree; if the conflicts are resolved within the set adjustment times, determining that the original temporary tasks are scheduled successfully, and outputting the adjusted scheduling scheme; otherwise, outputting the initial scheduling scheme.
Owner:CENT SOUTH UNIV

Relay satellite single-address antenna scheduling method suitable for breakpoint resumption

The invention discloses a relay satellite single-address antenna scheduling method suitable for breakpoint resumption. The method comprises the steps of obtaining a to-be-distributed task set; establishing a planning model of antenna scheduling, and defining an objective function and constraint conditions; allocating the tasks by adopting a two-stage scheduling algorithm, wherein the two-stage scheduling algorithm comprises a complete task distribution stage and a breakpoint resume task distribution stage, and the algorithm comprises the task resource matching, task available resource set generation, available time period conflict degree calculation, task insertion and operator updating by a task available resource set. The method of the invention aims to solve the problems of low task completion rate and low resource utilization rate caused by the difference of task requirements during the relay service process, considers the actual situation and the user requirements of the relay service at the same time and improves a traditional relay satellite application model, the algorithm can obtain a high-quality scheduling scheme within the shorter time, and is suitable for a relay satellite scheduling scene with higher requirements for scheduling time and has gains at the aspects of task completion rate, resource utilization rate and the like.
Owner:CENT SOUTH UNIV

Task satellite scheduling method for infrared LEO constellation

The invention relates to the technical field of aerospace, and provides a task satellite scheduling method for an infrared LEO constellation. The method comprises the following steps: projecting an invisible observation angle range of a satellite to a target to earth surface to obtain an undetectable range Db; projecting the maximum detection distance L of the satellite to the earth surface and removing the undetectable range Db to obtain a detectable range D1; projecting the target to the earth surface, and performing detectable analysis of the satellite and the target; screening orbital planes according to the longitude range of ascending nodes of the orbital planes and the geographic position of the target; and screening a task satellite from the screened orbital planes according to the relative motion relation between the satellite and the target and observable conditions. The problems that in the prior art, calculation is complex, on-satellite resource overhead is large and task planning timeliness is low in the task satellite scheduling process are at least partially solved, task satellite optimization efficiency and timeliness are improved, and the method has application value for task satellite scheduling of an infrared LEO constellation and design optimization of the constellation.
Owner:INNOVATION ACAD FOR MICROSATELLITES OF CAS +1

Satellite screening method and system based on task invitation

The invention provides a satellite screening method and system based on task invitation, and relates to the field of satellite scheduling. The method comprises the following steps: acquiring historical task data, wherein the historical task data comprise historical tasks and satellites corresponding to the historical tasks; acquiring a historical task demand vector based on the historical task; obtaining a to-be-observed task demand vector based on the to-be-observed task; obtaining the similarity between the historical task and the to-be-observed task based on the two demand vectors; obtaining a target historical task based on the similarity, and extracting a target satellite corresponding to the target historical task; inviting the target satellite based on the to-be-observed task; if the target satellite meets the energy constraint, the storage capacity constraint and the task time window constraint at the same time, enabling the target satellite to accept the invitation to obtain an invited satellite; if the number of the invited satellites is one, enabling the invited satellite to execute the task to be observed; and if the number of the inviting satellites is more than one, executing the task to be observed by the inviting satellite with the maximum income when the task to be observed is executed. The method and system are high in satellite screening efficiency.
Owner:HEFEI UNIV OF TECH

A task allocation method and system in a virtual constellation dynamic environment

The invention provides a task allocation method in a virtual constellation dynamic environment, and relates to the technical field of satellite scheduling. The method comprises the steps that when a virtual constellation management and control system receives a to-be-processed task, a meta-task set corresponding to the to-be-processed task is formed; the satellite platform searches an executable task set of each satellite in the management domain of the satellite platform and sends the executable task set of each satellite in the management domain of the satellite platform to the virtual constellation management and control system; a candidate meta-task subset formed by the executable meta-tasks of each satellite is determined in the management domain of the satellite platform; and the meta-task with the maximum expected revenue of each satellite in the candidate meta-task subset is used as the meta-task expected to bid by the satellite in the candidate meta-task subset; aiming at eachmeta-task in the meta-task set, the virtual constellation management and control system forms a candidate satellite set corresponding to the meta-task set; and an ordered satellite sequence corresponding to the meta-task is determined. According to the present invention, the task allocation efficiency can be improved.
Owner:HEFEI UNIV OF TECH

Single-satellite emergency mission planning method and system based on pointer neural network

The invention provides a pointer neural network-based single-satellite emergency task planning method and system, belonging to the technical field of satellite dispatching. The method includes forming multiple pieces of training data from the task requirement data set; generating an emergency task planning scheme; judging whether the number of iterations is greater than or equal to the number threshold; in the case of judging that the number of iterations is less than the number threshold, calculating the benefit; judging whether the number of iterations is equal to the initial value; when it is judged that the number of iterations is equal to the initial value, update the parameters according to the income; when it is judged that the number of iterations is not equal to the initial value, update the parameters according to the smoothed income; update the number of iterations; when it is judged that the number of iterations is greater than or equal to the number threshold, test The pointer neural network is used to judge whether the accuracy requirements are met; when the accuracy requirements are not met, the number of iterations is reset to the initial value; when the pointer neural network is judged to meet the accuracy requirements, the actual task requirements are received; the pointer neural network is used to generate emergency Mission planning scheme.
Owner:HEFEI UNIV OF TECH
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