CN111211831A - Multi-beam low-orbit satellite intelligent dynamic channel resource allocation method - Google Patents
Multi-beam low-orbit satellite intelligent dynamic channel resource allocation method Download PDFInfo
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Abstract
The invention relates to the technical field of air-space-earth-sea integrated communication, in particular to an intelligent dynamic channel resource allocation method for a multi-beam low-orbit satellite; the method takes a low earth orbit satellite as an Agent, maps the number of users requesting each wave beam service at the current service request moment and the initial state occupied by the wave beam to a channel as an environment, observes the environment state and acquires an environment reward signal by using a Q-learning algorithm according to the environment of the low earth orbit satellite at each service request moment, learns a state-action value function, gradually changes a channel resource allocation strategy, completes the dynamic channel resource allocation of the low earth orbit satellite mobile communication system, can avoid the allocation of the same channel resource to the users or the wave beams within a multiplexing distance, and realizes a channel resource allocation scheme which can enable the overall performance of the low earth orbit satellite mobile communication system to be optimal.
Description
Technical Field
The invention relates to the technical field of air-space-earth-sea integrated communication, in particular to an intelligent dynamic channel resource allocation method for a multi-beam low-orbit satellite.
Background
The air, space, ground and sea integrated information network is based on a ground network, is expanded by a space-based network, adopts a unified technical architecture, a unified technical system and a unified standard specification, is formed by interconnecting and intercommunicating a space-based information network, the internet and a mobile communication network, and has the characteristics of diversified service bearing, heterogeneous network interconnection, global resource management and the like. The air, space, ground and sea integrated information network is used as an important national information infrastructure and has important significance in a plurality of fields such as homeland security, emergency disaster relief, transportation, economic development and the like.
The low-orbit satellite communication is used as an important component in an air-space-earth-sea integrated information network and has the advantages of less transmission path loss, small communication time delay, wide coverage range, flexible access and the like. In the multi-beam low-orbit satellite mobile communication system, each satellite carries a plurality of beams, different beams can be utilized under the same frequency to meet frequency multiplexing to cover different areas on the ground, and the beams are combined together to complete the coverage of the ground visible area of a single satellite, so that the communication capacity is greatly increased. However, multi-beam low-orbit satellite communications also have some unavoidable problems. On one hand, when a user establishes a call, the user must access a channel in a certain beam of the satellite or switch from one beam to another beam, and in order to ensure that the communication is not interrupted, the user must be in the boundary of the coverage area of the adjacent beam, and a channel is allocated for the communication to complete the switching, so that the call can be ensured to be continuously carried out. On the other hand, satellite channel resources are limited, the demand of the channel resources is increasing along with the increasing number of communication users and the types of communication services, and the limited resources are managed and distributed by adopting scientific and effective measures, so that the satellite channel resources become a key for providing reliable services for users by a multi-beam low-orbit satellite communication system.
However, the low-earth satellite terminals are not uniformly distributed in the geographic space, so that the difference of communication traffic among beams of the low-earth satellite mobile communication system is large, and the demand of channel resources is different. If the fixed spectrum allocation mode is adopted, even if the user in the beam does not use the resource, other beam users cannot use the resource, and the waste of channel resources is easily caused. For the dynamic resource allocation mode, all channel resources can be used by each beam user, and the resource allocation is performed according to the number of service request users of each beam, so that the dynamic resource allocation mode has the advantage of higher resource utilization rate compared with a fixed frequency spectrum allocation mode. However, each beam user may use all channel resources, and the same channel may be allocated to a user in a short distance in the resource allocation process, thereby generating interference and affecting the communication service quality of the system.
Disclosure of Invention
Aiming at the defects in the prior art, the invention provides an intelligent dynamic channel resource allocation method for a multi-beam low-orbit satellite.
In one aspect, the present invention provides a method for allocating multi-beam low-earth orbit satellite intelligent dynamic channel resources, comprising the following steps:
s1, initializing a low-orbit satellite state-action value function Q (S, a), and setting an initial learning rate lambda and a discount factor β;
s2: the low-orbit satellite communication system forms N beams on the ground through satellite-borne multi-beam load, and the N beams are expressed as B ═ { N ═ 1,2, … N }; the available channel set C ═ { M ═ 1,2, … M }, where M is the number of channel resources; channel resource allocation state w for beam nn=[wn,1,wn,2,…,wn,M]Wherein each term wn,mE {0,1} represents the occupation situation of the beam n to the subchannel m, 1 represents occupation, and 0 represents idle and unoccupied; the channel allocation vectors of all beams in the low-earth satellite system form the total channel allocation matrix of the satellite system, which is W ═ W1,w2,…,wN](ii) a The channel resource matrix V ═ V [ V ] currently available for each beam1,v2,…,vN]Wherein v isn=[vn,1,vn,2,…,vn,M]Representing the available channel resource situation of each beam, the state of the t moment is constructed
S3: predicting actions to be taken by the low-orbit satellite according to the constructed state, and acquiring a Q value from a Q value characterization module of the low-orbit satellite;
s4: the low orbit satellite gathers a(s) from the feasible actions depending on the environment and state of the satellitet) Selecting the action with the maximum Q value according to the probability epsilon to execute;
s5: giving a reward function r after the low-orbit satellite reaches a termination state;
s6: the low-orbit satellite brings the state-action value function Q (s, a) into a Bellman formula for iterative updating, selects the next action according to the reward function r as estimation, and optimizes the state-action value function;
s7, when each iteration is finished, updating the discount factor β and judging whether the discount factor β is less than 0.01, if so, obtaining a channel distribution result Wt(ii) a If not, the process returns to step S6.
Optionally, the channel resource v available for each beam is selected from the group consisting of a plurality of beams, and a plurality of beams are arranged in a same beamnThe value and the represented meaning of each element in the vector are as follows:
optionally, the action atIs shown in state stSelecting a wave beam n from the available channel resource set, and allocating a channel resource m for the wave beam n, wherein the calculation expression is as follows: a ist={(n,m)|n,m∈Α(st),n∈B,m∈M}。
Optionally, the calculation expression of the state-action value function Q (s, a) substituted into the Bellman formula for iterative update is as follows: q(s)i,ai)=(1-λ)Q(si,ai)+λ(ri+βmaxQ(si,a))。
Optionally, the discount factor β needs to satisfy β e [0,1), which is set to gradually decrease with the learning process according to the negative exponential rule of e, so as to satisfy the convergence requirement of learning.
Optionally, the reward function r is designed as a scalar value positively correlated to the system performance, and the system performance is measured by using the system blocking probability, that is, the optimization target is that the number of blocked users of the system is minimum, and considering that at each service request time, a channel resource optimal allocation manner is learned according to the amount of users requesting the service of each beam, the designed reward function r should be correlated to the system performance in the termination state, so that a reward function r is given after the low-orbit satellite reaches the termination state, where the reward function r calculates an expression as follows:
wherein the content of the first and second substances,Rmaxthe maximum reward value represented is a scalar positive value; u shapeblockIndicating the number of current system blocking users, UallRepresenting the number of users in the system that request the service in total.
The invention has the beneficial effects that:
(1) the invention discloses a multi-beam low-orbit satellite intelligent dynamic channel resource allocation method, which is combined with a reinforcement learning algorithm in artificial intelligence, realizes dynamic allocation of low-orbit satellite communication system resources according to service requests of various beam users through state information of low-orbit satellites and the current communication environment, and improves the communication service performance of the system.
(2) According to the multi-beam low-orbit satellite intelligent dynamic channel resource allocation method, interference among users is considered when a dynamic resource allocation scheme is designed, and the influence of same frequency interference can be avoided.
(3) According to the intelligent dynamic channel resource allocation method for the multi-beam low-orbit satellite, the environment state is observed and the environment reward signal is acquired by using the Q-learning algorithm, the state-action value function is learned, the channel resource allocation strategy is changed step by step, and the learning speed and the learning effect of the system are greatly improved.
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In order to more clearly illustrate the detailed description of the invention or the technical solutions in the prior art, the drawings that are needed in the detailed description of the invention or the prior art will be briefly described below. Throughout the drawings, like elements or portions are generally identified by like reference numerals. In the drawings, elements or portions are not necessarily drawn to scale.
FIG. 1 is a schematic flow chart of an intelligent dynamic channel resource allocation method for a multi-beam low-orbit satellite according to the present invention;
fig. 2 is a diagram of the relationship between the system blocking rate and the traffic arrival rate under the condition of uniform traffic distribution.
Detailed Description
Embodiments of the present invention will be described in detail below with reference to the accompanying drawings. The following examples are only for illustrating the technical solutions of the present invention more clearly, and therefore are only examples, and the protection scope of the present invention is not limited thereby.
It is to be noted that, unless otherwise specified, technical or scientific terms used herein shall have the ordinary meaning as understood by those skilled in the art to which the invention pertains.
Reference herein to "an embodiment" means that a particular feature, structure, or characteristic described in connection with the embodiment can be included in at least one embodiment of the invention. The appearances of the phrase in various places in the specification are not necessarily all referring to the same embodiment, nor are separate or alternative embodiments mutually exclusive of other embodiments. It is explicitly and implicitly understood by one skilled in the art that the embodiments described herein can be combined with other embodiments.
At present, satellite channel resources are limited, and the demand of the channel resources is larger and larger as the number of communication users and the types of communication services are increased continuously; the low-orbit satellite terminals are unevenly distributed in the geographic space, so that the difference of communication traffic among beams of a low-orbit satellite mobile communication system is large; each beam user can use all channel resources, and the same channel can be allocated to users with close distance in the process of resource allocation, so that the problems of interference, influence on the communication service quality of the system and the like are caused; in order to solve the above problems, it is necessary to develop an intelligent dynamic channel resource allocation method for a multi-beam low-earth satellite, which observes an environment state and obtains an environmental reward signal by using a Q-learning algorithm, learns a state-action value function, gradually changes a channel resource allocation strategy, completes dynamic channel resource allocation of a low-earth satellite mobile communication system, can avoid allocating the same channel resource to users or beams within a multiplexing distance, and implements a channel resource allocation scheme capable of optimizing the overall performance of the low-earth satellite mobile communication system.
The specific implementation of the present invention provides a multi-beam low-orbit satellite intelligent dynamic channel resource allocation method, as shown in fig. 1-2, including the following steps:
in step S1, the low-earth satellite state-action value function Q (S, a) is initialized, and the initial learning rate λ and the discount factor β are set.
In the embodiment of the present invention, the step is the initialization of data, where s represents the state and a represents the action.
In step S2, the low earth orbit satellite communication system forms N beams on the ground by the satellite-borne multi-beam load, denoted as B ═ { N | N ═ 1,2, … N }; the available channel set C ═ { M ═ 1,2, … M }, where M is the number of channel resources; channel resource allocation state w for beam nn=[wn,1,wn,2,…,wn,M]Wherein each term wn,mE {0,1} represents the occupation situation of the beam n to the subchannel m, 1 represents occupation, and 0 represents idle and unoccupied; the channel allocation vectors of all beams in the low-earth satellite system form the total channel allocation matrix of the satellite system, which is W ═ W1,w2,…,wN](ii) a The channel resource matrix V ═ V [ V ] currently available for each beam1,v2,…,vN]Wherein v isn=[vn,1,vn,2,…,vn,M]Representing the available channel resource situation of each beam, the state of the t moment is constructed
In the embodiment of the present invention, the step is a component of a state, and the state is an abstraction of environment formalization and is also a basis for determining the executed action; channel resources v available for said respective beamnThe value and the represented meaning of each element in the vector are as follows:
in step S3, the low-earth satellite predicts an action to be taken based on the constructed state, and acquires a Q value from its own Q value characterization module.
In the embodiment of the invention, the step is the acquisition of the Q value, and in the step, in order to check the effectiveness of the algorithm, the predicted value of the prediction module is assumed to be accurate.
In step S4, the low orbit satellite aggregates a (S) from the set of feasible actions according to the environment and state of the satellitet) The action with the largest Q value is selected to be executed according to the probability epsilon.
In an embodiment of the invention, this step is the selection and execution of the action that the low orbiting satellite gets a(s) from the set of feasible actions depending on the environment and state it is int) Selecting the action with the maximum Q value according to the probability epsilon to execute; the action atIs shown in state stThe set of channel resources available at the bottom (i.e. state s)tThe element set with the median value of 0), selecting a beam n, and allocating a channel resource m for the beam n, wherein the calculation expression is as follows: e.g. of the type-xat={(n,m)|n,m∈Α(st),n∈B,m∈M}。
In step S5, a reward function r is given after each low-orbiting satellite reaches a termination state.
In the embodiment of the invention, the step is to obtain the return, the return is the feedback from the environment in the interactive process of the low-orbit satellite and the environment, the evaluation is carried out after the action is selected in a determined state, and the return is also an index for measuring the performance of the dynamic resource allocation algorithm; for convenience of calculation, the reward function r can be designed as a scalar value positively correlated to the system performance, and the system performance is measured by using the system blocking probability, that is, the optimization target is that the number of blocked users of the system is minimum, and in consideration of each service request moment, a channel resource optimal allocation mode is learned according to the amount of users requesting the service of each beam, the designed reward function r should be correlated to the system performance in the termination state, so that a reward function r is given after the low-orbit satellite reaches the termination state, wherein the reward function r calculates the expression as follows:
wherein R ismaxThe maximum reward value represented is a scalar positive value; u shapeblockIndicating the number of current system blocking users, UallRepresenting the number of users in the system that request the service in total.
In step S6, the low earth orbit satellite iteratively updates the state-action value function Q (S, a) into the Bellman equation, selects the next action based on the reward function r as an estimate, and optimizes the state-action value function.
In the embodiment of the invention, the step is the updating of the Q value; the calculation expression of the state-action value function Q (s, a) substituted into the Bellman formula for iterative updating is: q(s)i,ai)=(1-λ)Q(si,ai)+λ(ri+βmaxQ(si,a))。
In step S7, when each iteration is finished, the discount factor β is updated, and whether the discount factor β is smaller than 0.01 is determined, if yes, the channel allocation result W is obtainedt(ii) a If not, the process returns to step S6.
In the embodiment of the present invention, the step is parameter updating, the discount factor β needs to satisfy β e [0,1), it is set to gradually decrease with the learning process according to the negative exponential rule of e, and the expression is β -e-xWherein x is automatically added with 1 at the end of each iteration to meet the convergence requirement of learning, and when the requirement of the set discount factor β is met, a channel allocation result W is obtainedt。
The multi-beam low-orbit satellite intelligent dynamic Channel resource Allocation method is applied to practice, a multi-beam low-orbit satellite is assumed to be 54 beams, a service arrival model obeys Poisson distribution with a parameter of lambda, service duration obeys negative exponential distribution with a parameter of mu, the number of channels M is 204, a learning rate lambda is 0.005, a discount factor β is 0.90, and a maximum reward value is 100.
The invention has designed a multibeam low orbit satellite intelligence dynamic channel resource allocation method, this method regards low orbit satellite as Agent, every wave beam business under the present business request moment asks user's quantity and wave beam to initial state mapping that the channel occupies as the environment, under each business request moment, according to the environment that the low orbit satellite locates, utilize Q-learning algorithm to observe the environment state and obtain the reward signal of the environment, study the state-function of the action value, change the resource allocation tactics of the channel step by step, finish the dynamic channel resource allocation of the low orbit satellite mobile communication system, can avoid the same channel resource from allocating users or wave beams within the multiplexing distance, realize a can make the overall performance of the low orbit satellite mobile communication system reach the optimal channel resource allocation scheme; the method combines a reinforcement learning algorithm in artificial intelligence, realizes dynamic allocation of low-orbit satellite communication system resources according to service requests of each beam user through state information of the low-orbit satellite and the current communication environment, and improves the communication service performance of the system. The method considers the interference among users when designing the dynamic resource allocation scheme, and can avoid the influence of the same frequency interference. A Q-learning algorithm is utilized to observe the environment state and acquire the reward signals of the environment, a state-action value function is learned, a channel resource allocation strategy is changed step by step, and the learning speed and the learning effect of the system are greatly improved.
Finally, it should be noted that: the above embodiments are only used to illustrate the technical solution of the present invention, and not to limit the same; while the invention has been described in detail and with reference to the foregoing embodiments, it will be understood by those skilled in the art that: the technical solutions described in the foregoing embodiments may still be modified, or some or all of the technical features may be equivalently replaced; such modifications and substitutions do not depart from the spirit and scope of the present invention, and they should be construed as being included in the following claims and description.
Claims (6)
1. A multi-beam low-orbit satellite intelligent dynamic channel resource allocation method is characterized by comprising the following steps:
s1, initializing a low-orbit satellite state-action value function Q (S, a), and setting an initial learning rate lambda and a discount factor β;
s2: the low-orbit satellite communication system forms N beams on the ground through satellite-borne multi-beam load, and the N beams are expressed as B ═ { N ═ 1,2, … N }; the available channel set C ═ { M ═ 1,2, … M }, where M is the number of channel resources; channel resource allocation state w for beam nn=[wn,1,wn,2,…,wn,M]Wherein each term wn,mE {0,1} represents the occupation situation of the beam n to the subchannel m, 1 represents occupation, and 0 represents idle and unoccupied; the channel allocation vectors of all beams in the low-earth satellite system form the total channel allocation matrix of the satellite system, which is W ═ W1,w2,…,wN](ii) a The channel resource matrix V ═ V [ V ] currently available for each beam1,v2,…,vN]Wherein v isn=[vn,1,vn,2,…,vn,M]Representing the available channel resource situation of each beam, the state of the t moment is constructed
S3: predicting actions to be taken by the low-orbit satellite according to the constructed state, and acquiring a Q value from a Q value characterization module of the low-orbit satellite;
s4: the low orbit satellite gathers a(s) from the feasible actions depending on the environment and state of the satellitet) Selecting the action with the maximum Q value according to the probability epsilon to execute;
s5: giving a reward function r after the low-orbit satellite reaches a termination state;
s6: the low-orbit satellite brings the state-action value function Q (s, a) into a Bellman formula for iterative updating, selects the next action according to the reward function r as estimation, and optimizes the state-action value function;
s7, when each iteration is finished, updating the discount factor β and judging whether the discount factor β is less than 0.01, if so, obtaining a channel distribution result Wt(ii) a If not, the process returns to step S6.
3. the method of claim 1, wherein the action atIs shown in state stSelecting a wave beam n from the available channel resource set, and allocating a channel resource m for the wave beam n, wherein the calculation expression is as follows: a ist={(n,m)|n,m∈Α(st),n∈B,m∈M}。
4. The method of claim 1, wherein the state-action value function Q (s, a) is substituted into the calculation expression of Bellman's formula for iterative updating as: q(s)i,ai)=(1-λ)Q(si,ai)+λ(ri+βmaxQ(si,a))。
5. The method of claim 1, wherein the discount factor β is set to satisfy β e [0,1), and is gradually decreased along with the learning process according to the negative exponential rule of e to satisfy the convergence requirement of learning.
6. The method according to claim 1, wherein the reward function r is designed as a scalar positively correlated to the system performance, and the system performance is measured by the system blocking probability, that is, the optimization goal is that the number of blocked users of the system is minimum, and considering that at each service request time, an optimal channel resource allocation manner is learned according to the number of users requesting the service of each beam, the designed reward function r should be correlated to the system performance at the termination state, so that a reward function r is given after the low-orbit satellite reaches the termination state, wherein the reward function r calculates the expression as follows:
wherein R ismaxThe maximum reward value represented is a scalar positive value; u shapeblockIndicating the number of current system blocking users, UallRepresenting the number of users in the system that request the service in total.
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