CN110207708A - A kind of unmanned aerial vehicle flight path device for planning and method - Google Patents

A kind of unmanned aerial vehicle flight path device for planning and method Download PDF

Info

Publication number
CN110207708A
CN110207708A CN201910556400.3A CN201910556400A CN110207708A CN 110207708 A CN110207708 A CN 110207708A CN 201910556400 A CN201910556400 A CN 201910556400A CN 110207708 A CN110207708 A CN 110207708A
Authority
CN
China
Prior art keywords
grid
unmanned plane
flight path
aerial vehicle
unmanned aerial
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.)
Pending
Application number
CN201910556400.3A
Other languages
Chinese (zh)
Inventor
柴蓉
罗磊
陈前斌
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Chongqing University of Post and Telecommunications
Original Assignee
Chongqing University of Post and Telecommunications
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Chongqing University of Post and Telecommunications filed Critical Chongqing University of Post and Telecommunications
Priority to CN201910556400.3A priority Critical patent/CN110207708A/en
Publication of CN110207708A publication Critical patent/CN110207708A/en
Pending legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/20Instruments for performing navigational calculations

Abstract

The present invention relates to a kind of unmanned aerial vehicle flight path device for planning, belong to unmanned aerial vehicle flight path planning field.The device includes: geographical environment information collection module, unmanned plane characteristic perception module, information analysis module, flight path programming module, track optimization module;This method are as follows: geographical environment information collection module collects the possible flight range geographical environment information of unmanned plane, and is sent to information analysis module;Information analysis module analyzes zone state between the unmanned plane takeoff point and point of destination, obtain unmanned plane during flying danger zone information, and it is sent to flight path programming module, under conditions of considering global information, realize the planning and optimization to the unmanned aerial vehicle flight path.The invention further relates to a kind of unmanned aerial vehicle flight path planing methods.

Description

A kind of unmanned aerial vehicle flight path device for planning and method
Technical field
The invention belongs to unmanned aerial vehicle flight path planning field, it is related to a kind of unmanned aerial vehicle flight path device for planning and method.
Background technique
UAV abbreviation unmanned plane is manipulated using radio robot and the presetting apparatus provided for oneself Not manned vehicle.The advantages such as small in size, at low cost, the low and mobility strong of loss of unmanned plane make it be widely used in express delivery The industries such as service, city management, security be explosion-proof, agriculture, meteorological, electric power, rescue and relief work, video capture.Unmanned aerial vehicle flight path planning Refer to that based on unmanned plane mission requirements and flight range characteristic be unmanned plane optimization design flight path.The technology is to realize nobody Major issue of the machine in each field efficient application.
Research has been considered that unmanned aerial vehicle flight path planning problem, proposes to use based on Voronoi diagram if any document Dijkstra's algorithm finds unmanned plane optimal trajectory.Each unmanned plane threatening area is approximately a point by this method, chooses each prestige The intersection point of line perpendicular bisector is as track points between side of body point.This method can effectively ensure that track avoids each threat point.In another example There is document to propose to devise the group space to be developed by ant group algorithm based on ant group algorithm trajectory planning strategy and by group space The optimal belief space being deconstructed into, two spaces develop simultaneously, promote each other, so as to determine unmanned aerial vehicle flight path.However, nothing Since flight space range is big in man-machine practical application, parameter is more and parameter is directly interrelated, and mentioned algorithm is caused to be easy to fall into Enter locally optimal solution, optimal path can not be determined by even resulting in.It is examined in addition, the research of existing unmanned aerial vehicle flight path programme is less The design for considering trajectory planning device, causes mentioned algorithm to be limited in practical applications.
Summary of the invention
In view of this, being based on movement area the purpose of the present invention is to provide a kind of unmanned aerial vehicle flight path device for planning and method Domain geographical environment information, unmanned plane takeoff point, purpose dot position information plan unmanned plane under conditions of considering global information Track solves the problems, such as to fall into locally optimal solution during planning track.
In order to achieve the above objectives, the invention provides the following technical scheme:
On the one hand, a kind of unmanned aerial vehicle flight path device for planning is provided, comprising:
Geographical environment information collection module: the possible flight range geographical environment letter of unmanned plane is obtained based on numerical map Breath, and it is sent to information analysis module;
Unmanned plane characteristic perception module: perception unmanned plane takeoff point and purpose dot position information, unmanned plane current residual electricity Amount, unmanned plane during flying speed, maximum roll angle and minimum enroute I.F.R. altitude, and it is sent to information analysis module;
Information analysis module: receiving information collected by geographical environment information collection module, unmanned plane characteristic perception module, Zone state between unmanned plane takeoff point and point of destination is analyzed, obtains unmanned plane during flying danger zone information, and send To flight path programming module;
Flight path programming module: believed according to the information of information analysis module transmission and unmanned plane takeoff point, point of destination position Breath plans unmanned aerial vehicle flight path, and is sent to track optimization module;
Track optimization module: the unmanned aerial vehicle flight path planning strategy of flight path programming module output is received, judges whether to need to carry out Track optimization, if so, optimizing processing to track;Otherwise, without track optimization.
On the other hand, the present invention provides a kind of unmanned aerial vehicle flight path planing method, comprising:
The possible flight range geographical environment information of unmanned plane is obtained based on numerical map;
Perceive unmanned plane takeoff point and purpose dot position information, unmanned plane current residual electricity, unmanned plane minimum step, most Tight turn radius and minimum enroute I.F.R. altitude;
According to unmanned plane current electric quantity determine current maximum can flying distance, to area between unmanned plane takeoff point and point of destination Domain is analyzed, and unmanned plane during flying danger zone information is obtained;
According to unmanned plane takeoff point, purpose dot position information, unmanned plane during flying danger zone information planning unmanned aerial vehicle flight path;
According to the unmanned aerial vehicle flight path, judge whether that track optimization need to be carried out, if so, optimizing place to the track Reason;Conversely, without track optimization.
Further, the planning unmanned aerial vehicle flight path, specifically includes the following steps:
S1: unmanned plane during flying region modeling
To the unmanned plane during flying region carry out two-dimensional discrete, be modeled as two-dimensional grid, using the central point of grid as Track points enable X0, Y0Unmanned plane during flying zone level direction and vertical direction maximum distance are respectively indicated, Δ x, Δ y is enabled to distinguish table Show grid level direction and vertical direction discrete interval, thenQuantify space-number amount for grid level direction,For grid vertical direction quantized interval quantity, (m, n) indicates flight range grid, wherein 0≤m≤ Mmax,0≤n≤Nmax;I (m, n) is enabled to indicate the unmanned plane during flying region danger Marking the cell, if (m, n) is dangerous grid, I (m, n)=1;Otherwise, I (m, n)=0 enables the unmanned plane takeoff point be located at (ms,ns), point of destination is located at (md,nd);
S2: initialization opens, closes list
Enable the unmanned plane takeoff point (ms,ns) it is initial mesh, by initial mesh (ms,ns) be added to and open list Ls, That is Ls={ (ms,ns), remember ms=m0, ns=n0, claim (m0,n0) it is " father's grid ";It enables and closes list LcFor empty set, i.e. Lc= {Φ};
S3: adjacent mesh cost function is calculated
Find " father's grid " (m0, n0) all accessibility not dangerous grids in adjacent mesh, note (m, n) is (m0, n0) Adjacent mesh, i.e., | m-m0|=1 or | n-n0|=1, and I (m, n)=0, calculate (m0,n0) with the corresponding cost of track between (m, n) Function is denoted as fm,n, it is modeled as fm,n=gm,n+hm,n, wherein gm,nIt indicates from initial mesh (ms,ns) arrive (m, n) grid reality Cost, hm,nIt indicates the estimation cost from (m, n) grid to target gridding, records the f of (m, n)m,n、gm,nAnd hm,nValue;
S4: it updates and opens list and closing list
For accessibility grids all around " father's grid ", according to its fm,nIt is worth and descending sequentially adds unlatching list; If grid in opening list, is checked from initial mesh (ms,ns) pass through " father's grid " (m0, n0) reach grid (m, n) correspondence Gm,nValue, and with the current g of the gridm,nValue, is denoted asIt compares, ifThen by grid (m, n)It updates For gm,n, and recalculate grid fm,n;" father's grid " is deleted from unlatching list, is added to closing list;
S5: " father's grid " updates
It finds to open in list and corresponds to fm,nIt is worth minimum grid, is denoted as (m0, n0), enable it for " father's grid ";
S6: step S3-S5 is repeated
Step S3-S5 is repeated, until target gridding is added to closing list, since target gridding, You Geci " the father's grid " of iterative process dates back starting mesh, determines unmanned aerial vehicle flight path.
Further, g in step S3m,nIt is defined as (ms,ns) with the corresponding flight cost of track between (m, n), i.e., current " father Grid " actual cost g 'm,nWith it to the sum of corresponding flight cost of track between (m, n) grid, it is modeled as gm,n=C (| m-m0 |2+|n-n0|2)1/2+g′m,n, wherein C is unit grid cost, hm,nIt is defined as from (m, n) grid to level target gridding With the product of vertical grid quantity summation and unit grids cost, it is modeled as hm,n=C (| md-m|+|nd-n|)。
Further, three adjacent node angles are right angle to unmanned aerial vehicle flight path if it exists, then carry out track optimization processing, according to The unmanned plane during flying speed v, maximum roll angleBy formulaCalculate to obtain the unmanned plane minimum Turning radius, wherein g is acceleration of gravity, carries out track optimization based on gained turning radius.
The beneficial effects of the present invention are: the present invention is based on flight range geographical environment information, unmanned plane takeoff points, purpose Dot position information plans unmanned aerial vehicle flight path under conditions of considering global information, solves planning track and falls into part in the process The problem of optimal solution.
Other advantages, target and feature of the invention will be illustrated in the following description to a certain extent, and And to a certain extent, based on will be apparent to those skilled in the art to investigating hereafter, Huo Zheke To be instructed from the practice of the present invention.Target of the invention and other advantages can be realized by following specification and It obtains.
Detailed description of the invention
To make the objectives, technical solutions, and advantages of the present invention clearer, the present invention is made below in conjunction with attached drawing excellent The detailed description of choosing, in which:
Fig. 1 is trajectory planning schematic device of the present invention;
Fig. 2 is the flow diagram of path planning method of the present invention.
Specific embodiment
Illustrate embodiments of the present invention below by way of specific specific example, those skilled in the art can be by this specification Other advantages and efficacy of the present invention can be easily understood for disclosed content.The present invention can also pass through in addition different specific realities The mode of applying is embodied or practiced, the various details in this specification can also based on different viewpoints and application, without departing from Various modifications or alterations are carried out under spirit of the invention.It should be noted that diagram provided in following embodiment is only to show Meaning mode illustrates basic conception of the invention, and in the absence of conflict, the feature in following embodiment and embodiment can phase Mutually combination.
Wherein, the drawings are for illustrative purposes only and are merely schematic diagrams, rather than pictorial diagram, should not be understood as to this The limitation of invention;Embodiment in order to better illustrate the present invention, the certain components of attached drawing have omission, zoom in or out, not Represent the size of actual product;It will be understood by those skilled in the art that certain known features and its explanation may be omitted and be in attached drawing It is understood that.
The same or similar label correspond to the same or similar components in the attached drawing of the embodiment of the present invention;It is retouched in of the invention In stating, it is to be understood that if there is the orientation or positional relationship of the instructions such as term " on ", "lower", "left", "right", "front", "rear" To be based on the orientation or positional relationship shown in the drawings, be merely for convenience of description of the present invention and simplification of the description, rather than indicate or It implies that signified device or element must have a particular orientation, be constructed and operated in a specific orientation, therefore is described in attached drawing The term of positional relationship only for illustration, is not considered as limiting the invention, for the ordinary skill of this field For personnel, the concrete meaning of above-mentioned term can be understood as the case may be.
A kind of unmanned aerial vehicle flight path device for planning of the present invention and method, specifically: geographical environment information collection module The possible flight range geographical environment information of unmanned plane is collected, and is sent to information analysis module, information analysis module is to described Zone state is analyzed between unmanned plane takeoff point and point of destination, obtains unmanned plane during flying danger zone information, and be sent to Flight path programming module plans the unmanned aerial vehicle flight path under conditions of considering global information, solves planning track and falls into the process The problem of entering locally optimal solution.
Fig. 1 is trajectory planning schematic device of the present invention, as shown in Figure 1, the trajectory planning device includes: geographical ring Border information collection module: the possible flight range geographical environment information of unmanned plane is obtained based on numerical map, and is sent to information Analysis module;
Unmanned plane characteristic perception module: perceiving the unmanned plane takeoff point and purpose dot position information, and the unmanned plane is worked as Preceding remaining capacity, the unmanned plane during flying speed, maximum roll angle and minimum enroute I.F.R. altitude, and it is sent to information analysis mould Block;
Information analysis module: receiving information collected by geographical environment information collection module, unmanned plane characteristic perception module, Zone state between the unmanned plane takeoff point and point of destination is analyzed, unmanned plane during flying danger zone information is obtained, and It is sent to flight path programming module;
Flight path programming module: according to information analysis module and the unmanned plane takeoff point, purpose dot position information, institute is planned Unmanned aerial vehicle flight path is stated, and is sent to track optimization module;
Track optimization module: the unmanned aerial vehicle flight path planning strategy of flight path programming module output is received, judges whether to need to carry out Track optimization, if so, optimizing processing to the track;Otherwise, without track optimization.
Fig. 2 is the flow diagram of path planning method of the present invention, as shown in Fig. 2, trajectory planning of the present invention Method specifically: the possible flight range geographical environment information of unmanned plane is obtained based on numerical map;The unmanned plane is perceived to rise Flying spot and purpose dot position information, the unmanned plane current residual electricity, the unmanned plane minimum step, minimum turning radius and Minimum enroute I.F.R. altitude;Region between the unmanned plane takeoff point and point of destination is analyzed, unmanned plane during flying danger is obtained Danger zone domain information;According to the unmanned plane takeoff point, purpose dot position information, unmanned plane during flying danger zone information planning The unmanned aerial vehicle flight path, comprising:
To the unmanned plane during flying region carry out two-dimensional discrete, be modeled as two-dimensional grid, using the central point of grid as Track points enable X0, Y0Unmanned plane during flying zone level direction and vertical direction maximum distance are respectively indicated, Δ x, Δ y is enabled to distinguish table Show grid level direction and vertical direction discrete interval, thenQuantify space-number amount for grid level direction,For grid vertical direction quantized interval quantity, (m, n) indicates flight range grid, wherein 0≤m≤ Mmax,0≤n≤Nmax;I (m, n) is enabled to indicate the unmanned plane during flying region danger Marking the cell, if (m, n) is dangerous grid, I (m, n)=1;Otherwise, I (m, n)=0 enables the unmanned plane takeoff point be located at (ms,ns), point of destination is located at (md,nd)。
Enable the unmanned plane takeoff point (ms,ns) it is initial mesh, by initial mesh (ms,ns) be added to and open list Ls, That is Ls={ (ms,ns), remember ms=m0, ns=n0, claim (m0,n0) it is " father's grid ";It enables and closes list LcFor empty set, i.e. Lc= {Φ}。
Find " father's grid " (m0, n0) all accessibility not dangerous grids (m, n) in adjacent mesh, even | m-m0|=1 Or | n-n0|=1, and I (m, n)=0, calculate (m0,n0) with the corresponding cost function of track between (m, n), be denoted as fm,n, it is modeled as fm,n=gm,n+hm,n, wherein gm,nIt indicates from initial mesh (ms,ns)
To the actual cost of (m, n) grid, hm,nIt indicates the estimation cost from (m, n) grid to target gridding, records each The f of grid (m, n)m,n、gm,nAnd hm,nValue.
For accessibility grids all around " father's grid ", according to its fm,nIt is worth and descending sequentially adds unlatching list; If grid in opening list, is checked from initial mesh (ms,ns) pass through " father's grid " (m0, n0) reach grid (m, n) gm,nValue, and it is current with the gridValue is compared, ifThen grid (m, n)It is updated to gm,n, and again Calculate grid fm,n;" father's grid " is deleted from unlatching list, is added to closing list.
It finds to open in list and corresponds to fm,nIt is worth minimum grid, is denoted as (m0, n0), enable it for " father's grid ".
The above process is repeated, until target gridding is added to closing list.Since target gridding, repeatedly by each time Starting mesh is dateed back for " the father's grid " of process, that is, can determine unmanned aerial vehicle flight path.
According to the unmanned aerial vehicle flight path, judge whether that track optimization need to be carried out, if so, optimizing place to the track Reason;Conversely, without track optimization.
Finally, it is stated that the above examples are only used to illustrate the technical scheme of the present invention and are not limiting, although referring to compared with Good embodiment describes the invention in detail, those skilled in the art should understand that, it can be to skill of the invention Art scheme is modified or replaced equivalently, and without departing from the objective and range of the technical program, should all be covered in the present invention Scope of the claims in.

Claims (5)

1. a kind of unmanned aerial vehicle flight path device for planning, it is characterised in that: include:
Geographical environment information collection module: obtaining the possible flight range geographical environment information of unmanned plane based on numerical map, and It is sent to information analysis module;
Unmanned plane characteristic perception module: perception unmanned plane takeoff point and purpose dot position information, unmanned plane current residual electricity, nothing Man-machine flying speed, maximum roll angle and minimum enroute I.F.R. altitude, and it is sent to information analysis module;
Information analysis module: information collected by geographical environment information collection module, unmanned plane characteristic perception module is received, to nothing Zone state is analyzed between man-machine takeoff point and point of destination, obtains unmanned plane during flying danger zone information, and be sent to boat Mark planning module;
Flight path programming module: the information and unmanned plane takeoff point, purpose dot position information sent according to information analysis module, rule Unmanned aerial vehicle flight path is drawn, and is sent to track optimization module;
Track optimization module: the unmanned aerial vehicle flight path planning strategy of flight path programming module output is received, judges whether that track need to be carried out Optimization, if so, optimizing processing to track;Otherwise, without track optimization.
2. a kind of unmanned aerial vehicle flight path planing method, it is characterised in that: include:
The possible flight range geographical environment information of unmanned plane is obtained based on numerical map;
Perceive unmanned plane takeoff point and purpose dot position information, unmanned plane current residual electricity, unmanned plane minimum step, minimum turn Curved radius and minimum enroute I.F.R. altitude;
According to unmanned plane current electric quantity determine current maximum can flying distance, to region between unmanned plane takeoff point and point of destination into Row analysis, obtains unmanned plane during flying danger zone information;
According to unmanned plane takeoff point, purpose dot position information, unmanned plane during flying danger zone information planning unmanned aerial vehicle flight path;
According to the unmanned aerial vehicle flight path, judge whether that track optimization need to be carried out, if so, optimizing processing to the track; Conversely, without track optimization.
3. unmanned aerial vehicle flight path planing method according to claim 2, it is characterised in that: the planning unmanned aerial vehicle flight path, tool Body the following steps are included:
S1: unmanned plane during flying region modeling
Two-dimensional discrete is carried out to the unmanned plane during flying region, two-dimensional grid is modeled as, using the central point of grid as track Point, enables X0, Y0Unmanned plane during flying zone level direction and vertical direction maximum distance are respectively indicated, Δ x, Δ y is enabled to respectively indicate net Lattice horizontal direction and vertical direction discrete interval, thenQuantify space-number amount for grid level direction,For grid vertical direction quantized interval quantity, (m, n) indicates flight range grid, wherein 0≤m≤ Mmax,0≤n≤Nmax;I (m, n) is enabled to indicate the unmanned plane during flying region danger Marking the cell, if (m, n) is dangerous grid, I (m, n)=1;Otherwise, I (m, n)=0 enables the unmanned plane takeoff point be located at (ms,ns), point of destination is located at (md,nd);
S2: initialization opens, closes list
Enable the unmanned plane takeoff point (ms,ns) it is initial mesh, by initial mesh (ms,ns) be added to and open list Ls, i.e. Ls ={ (ms,ns), remember ms=m0, ns=n0, claim (m0,n0) it is " father's grid ";It enables and closes list LcFor empty set, i.e. Lc={ Φ };
S3: adjacent mesh cost function is calculated
Find " father's grid " (m0, n0) all accessibility not dangerous grids in adjacent mesh, note (m, n) is (m0, n0) it is adjacent Grid, i.e., | m-m0|=1 or | n-n0|=1, and I (m, n)=0, calculate (m0,n0) with the corresponding cost letter of track between (m, n) Number, is denoted as fm,n, it is modeled as fm,n=gm,n+hm,n, wherein gm,nIt indicates from initial mesh (ms,ns) arrive (m, n) grid practical generation Valence, hm,nIt indicates the estimation cost from (m, n) grid to target gridding, records the f of (m, n)m,n、gm,nAnd hm,nValue;
S4: it updates and opens list and closing list
For accessibility grids all around " father's grid ", according to its fm,nIt is worth and descending sequentially adds unlatching list;If net Lattice in opening list, are then checked from initial mesh (ms,ns) pass through " father's grid " (m0, n0) reach grid (m, n) it is corresponding gm,nValue, and with the current g of the gridm,nValue, is denoted asIt compares, ifThen by grid (m, n)It is updated to gm,n, and recalculate grid fm,n;" father's grid " is deleted from unlatching list, is added to closing list;
S5: " father's grid " updates
It finds to open in list and corresponds to fm,nIt is worth minimum grid, is denoted as (m0, n0), enable it for " father's grid ";
S6: step S3-S5 is repeated
Step S3-S5 is repeated, until target gridding is added to closing list, since target gridding, You Geci iteration " the father's grid " of process dates back starting mesh, determines unmanned aerial vehicle flight path.
4. unmanned aerial vehicle flight path planing method according to claim 3, it is characterised in that: g in step S3m,nIt is defined as (ms, ns) with the corresponding flight cost of track between (m, n), i.e., current " father's grid " actual cost g 'm,nWith its to (m, n) grid it Between the sum of the corresponding flight cost of track, be modeled as gm,n=C (| m-m0|2+|n-n0|2)1/2+g′m,n, wherein C is unit grid Cost, hm,nBe defined as from (m, n) grid to number of grid summation horizontal and vertical target gridding with unit grids cost it Product, is modeled as hm,n=C (| md-m|+|nd-n|)。
5. unmanned aerial vehicle flight path planing method according to claim 2, it is characterised in that: unmanned aerial vehicle flight path three phases if it exists Neighbors angle is right angle, then carries out track optimization processing, according to the unmanned plane during flying speed v, maximum roll angle By formulaCalculate to obtain the unmanned plane minimum turning radius, wherein g is acceleration of gravity, is based on gained Turning radius carries out track optimization.
CN201910556400.3A 2019-06-25 2019-06-25 A kind of unmanned aerial vehicle flight path device for planning and method Pending CN110207708A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201910556400.3A CN110207708A (en) 2019-06-25 2019-06-25 A kind of unmanned aerial vehicle flight path device for planning and method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201910556400.3A CN110207708A (en) 2019-06-25 2019-06-25 A kind of unmanned aerial vehicle flight path device for planning and method

Publications (1)

Publication Number Publication Date
CN110207708A true CN110207708A (en) 2019-09-06

Family

ID=67794361

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201910556400.3A Pending CN110207708A (en) 2019-06-25 2019-06-25 A kind of unmanned aerial vehicle flight path device for planning and method

Country Status (1)

Country Link
CN (1) CN110207708A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111006669A (en) * 2019-12-12 2020-04-14 重庆邮电大学 Unmanned aerial vehicle system task cooperation and path planning method
CN111578945A (en) * 2020-05-27 2020-08-25 福州尚易航农业科技有限公司 Unmanned aerial vehicle track planning method based on GNSS-machine vision
WO2021082396A1 (en) * 2019-11-01 2021-05-06 南京智慧航空研究院有限公司 Unmanned aerial vehicle flight network modeling method based on low-altitude airspace restriction conditions
CN115953919A (en) * 2023-03-15 2023-04-11 国科星图(深圳)数字技术产业研发中心有限公司 Flight management system and method based on gridding air route analysis

Citations (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102880186A (en) * 2012-08-03 2013-01-16 北京理工大学 Flight path planning method based on sparse A* algorithm and genetic algorithm
CN103697896A (en) * 2014-01-13 2014-04-02 西安电子科技大学 Unmanned aerial vehicle route planning method
US20160202695A1 (en) * 2014-09-12 2016-07-14 4D Tech Solutions, Inc. Unmanned aerial vehicle 3d mapping system
CN105953800A (en) * 2016-06-14 2016-09-21 北京航空航天大学 Route planning grid space partitioning method for unmanned aerial vehicle
CN106203721A (en) * 2016-07-18 2016-12-07 武汉理工大学 Ice formation, the polar region flight-line design system and method for self-adaptive ship ice-breaking capacity
CN106441303A (en) * 2016-09-30 2017-02-22 哈尔滨工程大学 Path programming method based on A* algorithm capable of searching continuous neighborhoods
CN106687876A (en) * 2014-07-14 2017-05-17 A·贾雷尔 约翰 Unmanned aerial vehicle communication, monitoring, and traffic management
CN107345815A (en) * 2017-07-24 2017-11-14 东北大学 A kind of home-services robot paths planning method based on improvement A* algorithms
CN107677273A (en) * 2017-09-11 2018-02-09 哈尔滨工程大学 A kind of cluster unmanned plane Multiple routes planning method based on two-dimensional grid division
CN108274465A (en) * 2018-01-10 2018-07-13 上海理工大学 Based on optimization A*Artificial Potential Field machinery arm, three-D obstacle-avoiding route planning method
CN108592925A (en) * 2018-07-26 2018-09-28 中国人民解放军陆军工程大学 Unmanned plane turning Path Planning based on min. turning radius
US20180308371A1 (en) * 2017-04-19 2018-10-25 Beihang University Joint search method for uav multiobjective path planning in urban low altitude environment
CN108846522A (en) * 2018-07-11 2018-11-20 重庆邮电大学 UAV system combines charging station deployment and route selection method
CN108932876A (en) * 2018-08-14 2018-12-04 湖北工业大学 A kind of express delivery unmanned aerial vehicle flight path planing method of the A* introducing black area and ant colony algorithm
CN108958285A (en) * 2018-07-17 2018-12-07 北京理工大学 It is a kind of that path planning method is cooperateed with based on the efficient multiple no-manned plane for decomposing thought
CN109582035A (en) * 2018-11-29 2019-04-05 沈阳无距科技有限公司 A kind of aircraft's flight track air navigation aid, device and electronic equipment
CN109670656A (en) * 2019-02-27 2019-04-23 重庆邮电大学 A kind of unmanned plane optimal communication route planning method based on 4G network

Patent Citations (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102880186A (en) * 2012-08-03 2013-01-16 北京理工大学 Flight path planning method based on sparse A* algorithm and genetic algorithm
CN103697896A (en) * 2014-01-13 2014-04-02 西安电子科技大学 Unmanned aerial vehicle route planning method
CN106687876A (en) * 2014-07-14 2017-05-17 A·贾雷尔 约翰 Unmanned aerial vehicle communication, monitoring, and traffic management
US20160202695A1 (en) * 2014-09-12 2016-07-14 4D Tech Solutions, Inc. Unmanned aerial vehicle 3d mapping system
CN105953800A (en) * 2016-06-14 2016-09-21 北京航空航天大学 Route planning grid space partitioning method for unmanned aerial vehicle
CN106203721A (en) * 2016-07-18 2016-12-07 武汉理工大学 Ice formation, the polar region flight-line design system and method for self-adaptive ship ice-breaking capacity
CN106441303A (en) * 2016-09-30 2017-02-22 哈尔滨工程大学 Path programming method based on A* algorithm capable of searching continuous neighborhoods
US20180308371A1 (en) * 2017-04-19 2018-10-25 Beihang University Joint search method for uav multiobjective path planning in urban low altitude environment
CN107345815A (en) * 2017-07-24 2017-11-14 东北大学 A kind of home-services robot paths planning method based on improvement A* algorithms
CN107677273A (en) * 2017-09-11 2018-02-09 哈尔滨工程大学 A kind of cluster unmanned plane Multiple routes planning method based on two-dimensional grid division
CN108274465A (en) * 2018-01-10 2018-07-13 上海理工大学 Based on optimization A*Artificial Potential Field machinery arm, three-D obstacle-avoiding route planning method
CN108846522A (en) * 2018-07-11 2018-11-20 重庆邮电大学 UAV system combines charging station deployment and route selection method
CN108958285A (en) * 2018-07-17 2018-12-07 北京理工大学 It is a kind of that path planning method is cooperateed with based on the efficient multiple no-manned plane for decomposing thought
CN108592925A (en) * 2018-07-26 2018-09-28 中国人民解放军陆军工程大学 Unmanned plane turning Path Planning based on min. turning radius
CN108932876A (en) * 2018-08-14 2018-12-04 湖北工业大学 A kind of express delivery unmanned aerial vehicle flight path planing method of the A* introducing black area and ant colony algorithm
CN109582035A (en) * 2018-11-29 2019-04-05 沈阳无距科技有限公司 A kind of aircraft's flight track air navigation aid, device and electronic equipment
CN109670656A (en) * 2019-02-27 2019-04-23 重庆邮电大学 A kind of unmanned plane optimal communication route planning method based on 4G network

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
周璐: "具有方向约束的无人机动态航迹规划研究", 《中国优秀博硕士学位论文全文数据库(硕士)工程科技Ⅱ辑》 *
姜文: "电力巡线系统四轴飞行器自动避障研究", 《中国优秀博硕士学位论文全文数据库(硕士)工程科技Ⅱ辑》 *
胡云舒: "无人机航路规划系统研究", 《中国优秀博硕士学位论文全文数据库(硕士)工程科技Ⅱ辑》 *

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2021082396A1 (en) * 2019-11-01 2021-05-06 南京智慧航空研究院有限公司 Unmanned aerial vehicle flight network modeling method based on low-altitude airspace restriction conditions
CN111006669A (en) * 2019-12-12 2020-04-14 重庆邮电大学 Unmanned aerial vehicle system task cooperation and path planning method
CN111578945A (en) * 2020-05-27 2020-08-25 福州尚易航农业科技有限公司 Unmanned aerial vehicle track planning method based on GNSS-machine vision
CN115953919A (en) * 2023-03-15 2023-04-11 国科星图(深圳)数字技术产业研发中心有限公司 Flight management system and method based on gridding air route analysis

Similar Documents

Publication Publication Date Title
CN110207708A (en) A kind of unmanned aerial vehicle flight path device for planning and method
Almadhoun et al. A survey on multi-robot coverage path planning for model reconstruction and mapping
CN106873628B (en) A kind of collaboration paths planning method of multiple no-manned plane tracking multimachine moving-target
CN103913172B (en) A kind of it is applicable to the paths planning method of aircraft under complicated low latitude
CN106125764B (en) Based on A*The unmanned plane path dynamic programming method of search
Yu et al. Cooperative path planning for target tracking in urban environments using unmanned air and ground vehicles
CN102129249B (en) Method for planning global path of robot under risk source environment
Dang et al. Autonomous exploration and simultaneous object search using aerial robots
CN107807665B (en) Unmanned aerial vehicle formation detection task cooperative allocation method and device
CN105841702A (en) Method for planning routes of multi-unmanned aerial vehicles based on particle swarm optimization algorithm
Song et al. Online inspection path planning for autonomous 3D modeling using a micro-aerial vehicle
Basiri et al. A survey on the application of path-planning algorithms for multi-rotor UAVs in precision agriculture
CN105045274B (en) A kind of intelligent shaft tower connected graph construction method for unmanned plane inspection trajectory planning
CN106197426A (en) A kind of unmanned plane emergency communication paths planning method and system
CN104407619A (en) Method enabling multiple unmanned aerial vehicles to reach multiple targets simultaneously under uncertain environments
CN104155998B (en) A kind of path planning method based on potential field method
CN109656264A (en) For being generated to the method implemented by computer and system in the path 3D in landing site for aircraft
CN110349445A (en) Aerial flight section with multiple RTA constraint
Geng et al. UAV surveillance mission planning with gimbaled sensors
Li et al. Multi-robot mission planning with static energy replenishment
Peng et al. Three-dimensional multi-constraint route planning of unmanned aerial vehicle low-altitude penetration based on coevolutionary multi-agent genetic algorithm
Yoon et al. Collaborative mission and route planning of multi-vehicle systems for autonomous search in marine environment
CN107422734B (en) Robot path planning method based on chaotic reverse pollination algorithm
CN111506078B (en) Robot navigation method and system
Sisso et al. Info-gap approach to multiagent search under severe uncertainty

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
RJ01 Rejection of invention patent application after publication

Application publication date: 20190906

RJ01 Rejection of invention patent application after publication