CN105182449B

CN105182449B - DATA REASONING acquisition methods, apparatus and system

Info

Publication number: CN105182449B
Application number: CN201510532675.5A
Authority: CN
Inventors: 不公告发明人
Original assignee: Dongguan Frontier Technology Institute; Shenzhen Kuang Chi Space Technology Co Ltd
Current assignee: Dongguan Dongguan Institute Of Science And Technology Innovation
Priority date: 2015-08-26
Filing date: 2015-08-26
Publication date: 2018-07-03
Anticipated expiration: 2035-08-26
Also published as: CN105182449A

Abstract

The invention discloses a kind of DATA REASONING acquisition methods, apparatus and systems.Wherein, which includes：Main aerostatics node, from aerostatics node and ground control station, wherein, main aerostatics node is communicated to connect with multiple established from aerostatics node, multiple from aerostatics node motion to corresponding measurement position for controlling, and is obtained and analyzed multiple measurement data from aerostatics node in measurement position；Ground control station is established with main aerostatics node and is communicated to connect, and controls main aerostatics node instruction is described to perform measurement task from aerostatics node for passing through.The present invention is solved since the fixation of surface-based observing station causes to survey the technical issues of demeanour encloses measurement range that is small and then limiting upper air wind measuring.

Description

DATA REASONING acquisition methods, apparatus and system

Technical field

The present invention relates to communication technology application fields, in particular to a kind of DATA REASONING acquisition methods, device and are System.

Background technology

High-altitude wind measurement at present, it is main to be carried out using wind aerostatics is surveyed, it is floated by ground with pilot balloon theodolite to surveying wind The continuous tracking observation of pocket, and write down and survey wind the aerostatics elevation angle and azimuth per minute, floating then is obtained by calculating The mean wind direction and wind speed for aerial each layer that device passes through.But when at present to high-altitude wind measurement, ground theodolite needs first Manual record observes data, and secondly manual entry data, finally manually by the data to typing carry out that upper-level winds is calculated Measurement result, entire measurement process program is cumbersome as from the foregoing, and several surveyors is needed to cooperate with and are carried out, therefore due to synchronous and real When property is all difficult to ensure that, and can only carry out the measuring wind speed of certain area over a period to come, if region is changed if need The related ground installations such as artificial mobile theodolite, so as to which a large amount of human and material resources can be expended, and since various regions are frequent The meteorological conditions such as the haze that will appear can influence the application of pilot balloon theodolite, therefore larger not side can be brought to high-altitude wind measurement Just.

Therefore, how improving measurement accuracy, improve measurement efficiency become this cause important topic to be solved it One.

It is specific as follows there are two kinds of settling modes in existing realization method：

Mode one, provides a kind of wind measuring system of the double electronic optical theodolite of semi-automation, which can automate and adopt Collect data；

Mode two provides a kind of aerological sounding GPS wind detection units, has low cost, reliable and stable, is not required to very important person The advantages of work tracks；

But artificial tracking aerostatics is needed in mode one in upper air wind measuring, bring mistake due to manually tracking meeting subjectivity Difference, so as to cause surveying, wind precision is low；Mode two is enclosed since surface-based observing station is fixed, so can not expand and survey demeanour, limits height Sky surveys the measurement range of wind.

Survey demeanour is caused to enclose measurement model that is small and then limiting upper air wind measuring for the above-mentioned fixation due to surface-based observing station The problem of enclosing, currently no effective solution has been proposed.

Invention content

An embodiment of the present invention provides a kind of DATA REASONING acquisition methods, apparatus and system, at least to solve due to ground The fixation of observation station causes to survey the technical issues of demeanour encloses measurement range that is small and then limiting upper air wind measuring.

One side according to embodiments of the present invention provides a kind of DATA REASONING and obtains system, including：Main aerostatics section Point, from aerostatics node and ground control station, wherein, main aerostatics node with it is multiple from aerostatics node establish communicate to connect, It is multiple from aerostatics node motion to corresponding measurement position for controlling, and obtain analysis and multiple measured from aerostatics node The measurement data of position；Ground control station is established with main aerostatics node and is communicated to connect, and main aerostatics node is controlled for passing through Instruction is described to perform measurement task from aerostatics node.

Another aspect according to embodiments of the present invention additionally provides a kind of DATA REASONING acquisition methods, applied to above-mentioned number According to measure acquisition system, including：Control instruction is sent from aerostatics node to any one or more, control instruction is used to indicate From the measurement position of aerostatics node and/or perform the corresponding measurement task for measuring position；Reception is being measured from aerostatics node The measurement data for the measurement task that position is sent；Measurement data is analyzed, obtains the measurement result of corresponding measurement data.

Another aspect according to embodiments of the present invention additionally provides a kind of DATA REASONING acquisition methods, applied to above-mentioned number According to measure acquisition system, including：The control instruction that main aerostatics node is sent is received, control instruction, which is used to indicate, measures position, And/or perform the corresponding measurement task for measuring position；It is performed according to the position that measures in control instruction in the measurement for measuring position Task；To the measurement data of main aerostatics node return measurement task.

Another aspect according to embodiments of the present invention additionally provides a kind of DATA REASONING acquisition device, including：Send mould Block, for sending control instruction from aerostatics node to any one or more, control instruction is used to indicate from aerostatics node Measurement position and/or perform the corresponding measurement task for measuring position；First receiving module, for receiving from aerostatics node In the measurement data for measuring the measurement task that position is sent；Measurement module for analyzing measurement data, obtains corresponding survey Measure the measurement result of data.

Another aspect according to embodiments of the present invention additionally provides a kind of DATA REASONING acquisition device, including：Command reception Module, for receiving the control instruction that main aerostatics node is sent, control instruction, which is used to indicate, measures position and/or execution pair The measurement task of position should be measured；Measurement module, for being performed according to the position that measures in control instruction in the survey for measuring position Amount task；Data transmission blocks, for the measurement data of main aerostatics node return measurement task.

In embodiments of the present invention, it is controlled using main aerostatics node to any one or more sent from aerostatics node Instruction, control instruction are used to indicate from aerostatics node measurement position and/or perform the corresponding measurement task for measuring position；It connects It receives from aerostatics node in the measurement data for measuring the measurement task that position is sent；DATA REASONING behaviour is performed according to measurement data Make, achieved the purpose that measurement range can be changed automatically according to measurement task, it is achieved thereby that promoting upper air wind measuring efficiency Technique effect, and then solve since the fixation of surface-based observing station causes survey demeanour to enclose measurement that is small and then limiting upper air wind measuring The technical issues of range.

Description of the drawings

Attached drawing described herein is used to provide further understanding of the present invention, and forms the part of the application, this hair Bright illustrative embodiments and their description do not constitute improper limitations of the present invention for explaining the present invention.In the accompanying drawings：

Fig. 1 is the structure chart that DATA REASONING according to embodiments of the present invention obtains system；

Fig. 2 is the structure chart of main aerostatics node in DATA REASONING acquisition system according to embodiments of the present invention；

Fig. 3 is the first communication terminal in main aerostatics node in DATA REASONING acquisition system according to embodiments of the present invention Structure chart；

Fig. 4 is from the structure chart of aerostatics node in DATA REASONING acquisition system according to embodiments of the present invention；

Fig. 5 be in DATA REASONING acquisition system according to embodiments of the present invention from aerostatics node the second communication terminal Structure chart；

Fig. 6 is the flow chart of DATA REASONING acquisition methods according to embodiments of the present invention；

Fig. 7 is the flow chart of DATA REASONING acquisition methods according to embodiments of the present invention；

Fig. 8 is the structure diagram of according to embodiments of the present invention two DATA REASONING acquisition device；

Fig. 9 is a kind of structure diagram of according to embodiments of the present invention two DATA REASONING acquisition device；

Figure 10 is the structure diagram of according to embodiments of the present invention two another DATA REASONING acquisition device；

Figure 11 is the structure diagram of according to embodiments of the present invention two another DATA REASONING acquisition device；

Figure 12 is the structure diagram of according to embodiments of the present invention two another DATA REASONING acquisition device；

Figure 13 is the structure diagram of according to embodiments of the present invention two another DATA REASONING acquisition device；

Figure 14 is the structure diagram of according to embodiments of the present invention three DATA REASONING acquisition device；

Figure 15 is a kind of structure diagram of according to embodiments of the present invention three DATA REASONING acquisition device；

Figure 16 is the structure diagram of according to embodiments of the present invention three another DATA REASONING acquisition device；

Figure 17 is the structure diagram of according to embodiments of the present invention three another DATA REASONING acquisition device；And

Figure 18 is the structure diagram of according to embodiments of the present invention three another DATA REASONING acquisition device.

Specific embodiment

In order to which those skilled in the art is made to more fully understand the present invention program, below in conjunction in the embodiment of the present invention The technical solution in the embodiment of the present invention is clearly and completely described in attached drawing, it is clear that described embodiment is only The embodiment of a part of the invention, instead of all the embodiments.Based on the embodiments of the present invention, ordinary skill people Member's all other embodiments obtained without making creative work should all belong to the model that the present invention protects It encloses.

It should be noted that term " first " in description and claims of this specification and above-mentioned attached drawing, " Two " etc. be the object for distinguishing similar, and specific sequence or precedence are described without being used for.It should be appreciated that it uses in this way Data can be interchanged in the appropriate case, so as to the embodiment of the present invention described herein can in addition to illustrating herein or Sequence other than those of description is implemented.In addition, term " comprising " and " having " and their any deformation, it is intended that cover Cover it is non-exclusive include, be not necessarily limited to for example, containing the process of series of steps or unit, method, system, product or equipment Those steps or unit clearly listed, but may include not listing clearly or for these processes, method, product Or the intrinsic other steps of equipment or unit.

Embodiment 1

An embodiment of the present invention provides a kind of DATA REASONINGs to obtain system.

Fig. 1 is the structure chart that DATA REASONING according to embodiments of the present invention obtains system.As shown in Figure 1, the DATA REASONING Acquisition system includes as follows：Main aerostatics node 12, from aerostatics node 14 and ground control station 16, wherein,

Main aerostatics node 12 is communicated to connect with multiple established from aerostatics node 14, multiple from aerostatics section for controlling Point 14 is moved to corresponding measurement position, and obtains and analyze multiple measurement numbers from aerostatics node 14 in corresponding measurement position According to；Ground control station 16 and main aerostatics node 12, which are established, to be communicated to connect, for pass through control main aerostatics node 12 indicate from Aerostatics node 14 performs measurement task.

Specifically, main aerostatics node 12 and be mobile node from aerostatics node 14, ground control station 16 is fixed knot Point, ground control station 16, which is mainly used to establish with main aerostatics node 12, to be communicated to connect, and is obtained according to prefixed time interval main floating The location information of pocket node 12, to send emergency flight control instruction to main aerostatics node 12 if necessary, in main aerostatics Node 12 and after the lift-off of aerostatics node 14, main aerostatics node 12 is that entire DATA REASONING obtains system (that is, distributed high Air balls wind measuring system) control centre, wherein, main 12 function of aerostatics node mainly include three aspect, first aspect be with It communicates from aerostatics node 14, obtains the velocity information from the current location of aerostatics node 14 and corresponding current location； Second aspect is in executive control operation, and control instruction is sent to from aerostatics node 14；The third aspect is obtained from floating The response message for the destination locations that device node 14 is set after control instruction is received in control instruction is arrived at and the arrival purpose The headway data of position.It is the execution that DATA REASONING obtains system by multiple test clusters formed from aerostatics node 14 System, flight position, the corresponding speed of the position and time point data when function mainly includes acquisition without control flight, and it is fixed The antenna transmission that phase establishes antenna L frequency ranges with main aerostatics node 12 links, and by current location, corresponds to the speed of current location, Time point data passes through L frequency range wireless transmissions to main aerostatics node 12.

From the foregoing, it will be observed that sending control instruction to from aerostatics node 14 using main aerostatics node 12, control instruction is used for It indicates from aerostatics node measurement position and/or performs the corresponding measurement task for measuring position；Reception exists from aerostatics node 14 Measure the measurement data for the measurement task that position is sent；Main aerostatics node 12 carries out analysis and arrangement to measurement data, is somebody's turn to do The corresponding measurement result of measurement data, having reached can be according to measurement task certainly from aerostatics node 14 during upper air wind measuring The dynamic purpose for changing measurement range, it is achieved thereby that promoting the technique effect of upper air wind measuring efficiency, and then solves due to ground The fixation of observation station causes to survey the technical issues of demeanour encloses measurement range that is small and then limiting upper air wind measuring.

Preferably, Fig. 2 is the structure chart of main aerostatics node in DATA REASONING acquisition system according to embodiments of the present invention. As shown in Fig. 2, main aerostatics node 12 includes：First computer 121, the first power plant 122, the first communication terminal 123, One aerostatics 124 and first vector 125, wherein,

First vector 125 is for the first computer 121 of carrying, the first power plant 122 and the first communication terminal 123.

First computer 121 and the first power plant 122 and the first communication terminal 123 establish communication connection respectively, are used for By the way that the first power plant 122 is controlled to rise to preset height or determining current air position, by controlling the first communication terminal 123 communicate with ground control station 16 or from aerostatics node 14, and store the measurement data sent from aerostatics node, In, the first power plant 122 is propeller arrangement power plant；

Specifically, the first computer 121 is risen or fallen for the first power plant 122 of control to first computer 121 setting height or in the air when main aerostatics node 12 aerial statue；First computer 121 is dynamic except control first Outside power apparatus 122, be additionally operable to the first communication terminal 123 of control with from aerostatics node 14 and with ground control station 16 respectively into Row communication.

First computer 121 except have the function of it is above-mentioned in addition to, the first computer 121 is also equipped with storing or calculate by first The function for the measurement data that the slave aerostatics node 14 that communication terminal 123 receives is sent, wherein, to ensure the first computer 121 can normal operation, mitigate computational burden, the first computer in DATA REASONING acquisition system provided in an embodiment of the present invention 121, to store the measurement data sent from aerostatics node 14 as preferred embodiment, ground control station 16 are transferred to after ground is returned to It carries out calculation processing or is sent out the slave aerostatics node 14 received according to predetermined time interval by the first communication terminal 123 The measurement data sent is sent to ground control station 16, and calculation processing is carried out to data, and then reach in time by ground control station 16 Promote the efficiency of Measurement and Data Processing.

First aerostatics 124 is connect with first vector 125, for providing aerostatic buoyancy for first vector 125；Wherein, One aerostatics 124 can be aerological balloon, so that providing the aerostatic buoyancy of rising for first vector 125.

Specifically, the first aerostatics 124 is connect with first vector 125, the active force as entire main aerostatics node 12 Source provides buoyancy for the rising of main aerostatics node.Wherein, first vector 125 can be the structure of hanging basket.

Preferably, Fig. 3 is first logical in main aerostatics node in DATA REASONING acquisition system according to embodiments of the present invention Believe the structure chart of terminal.As shown in figure 3, the first communication terminal 123 includes：First communication device 1231 and secondary communication device 1232, wherein,

First communication device 1231 is used to send control instruction from aerostatics node 14 to any one or more；

Secondary communication device 1232 is used to receive any one or more measurement data returned from aerostatics node.

Specifically, in the first communication terminal 123, first communication device 1231 refers to for the low control of transmission data amount demand It enabling, secondary communication device 1232 is used to receive the high measurement data of data volume demand, wherein, first communication device 1231 can be According to satellite communication equipments such as star communication terminals, control instruction is sent；Secondary communication device 1232 is due to being used for transmission from aerostatics The measurement data of node 14, it is distinct all with first communication device 1231 for the stability, promptness and capacity of channel And have higher requirement, so secondary communication device 1232 can pass through when realizing transmitting-receiving from the measurement data of aerostatics node Radio wave, as L-band carries out the transmission of big data transfers, especially measurement data.

Preferably, Fig. 4 is from the structure chart of aerostatics node in DATA REASONING acquisition system according to embodiments of the present invention. As shown in figure 4, include from aerostatics node 14：Second computer 141, the second power plant 142, the second communication terminal 143, Two aerostatics 144 and Second support 145, wherein, Second support 145 is used to carry second computer 141, the second power plant 142 and second communication terminal 143；

Specifically, from 125 work(of first vector in the Second support 145 in aerostatics node 14 and main aerostatics node 12 Can be identical, details are not described herein again, is to ensure the basic guarantee that DATA REASONING is completed from aerostatics node 14.Wherein, Second support 145 can be the structure of hanging basket.141 and second power plant 142 of second computer and the second communication terminal 143 establish communication link It connects, for the control instruction of main aerostatics node 12 received according to the second communication terminal 143, so that referring to according to the control It enables the second power plant 142 of control that will be driven from aerostatics node 14 and reaches scheduled measurement position, and it is logical to pass through second Believe that terminal 143 sends measurement data to main aerostatics node 12, wherein, the second power plant 142 is filled for propeller arrangement power It puts；

Specifically, second computer 141 is from the control function element in aerostatics node 14, for controlling second respectively 142 and second communication terminal 143 of power plant, wherein, second computer 141 controls the second power plant 142 according to main floating The control instruction of device node 12 rises or reaches position as defined in the control instruction and keeps from the aerial of aerostatics node 14 Posture；Second computer 141 control the second communication terminal 143 be in order to ensure ensure between main aerostatics node 12 it is unimpeded Communication connection ensures the normal transmitting-receiving of control instruction and data transmission, is the root that DATA REASONING is completed from aerostatics node 14 This guarantee.

Second aerostatics 144 is connect with Second support 145, for providing aerostatic buoyancy for Second support 145；Wherein, Two aerostatics 144 can be aerological balloon, so that providing the aerostatic buoyancy of rising for Second support 145.

Specifically, the second aerostatics 144 is entirely provides main power source from aerostatics node 14, it is from aerostatics node It rises and buoyancy is provided.

Preferably, Fig. 5 is second logical from aerostatics node in DATA REASONING acquisition system according to embodiments of the present invention Believe the structure chart of terminal.As shown in figure 5, the second communication terminal 143 includes：Third communication device 1431 and fourth communication device 1432, wherein,

Third communication device 1431 is used to receive the control instruction that main aerostatics node 12 is sent；

Fourth communication device 1432 is used for main 12 return measurement data of aerostatics node.

Specifically, third communication device 1431 corresponds to the first communication device 1231 in main aerostatics node 12, for connecing Receive the control instruction of first communication device 1231；Fourth communication device 1432 corresponds to the second communication dress in main aerostatics node 12 1232 are put, after receiving for the test instruction of test, four-way will be passed through according to the measurement data obtained after test instruction T unit 1432 is sent to the secondary communication device 1232 in main aerostatics node 12.

Herein it should be noted that the first power plant 122 in main aerostatics node 12 provided in an embodiment of the present invention with Can be the power plant of propeller arrangement from the second power plant 142 in aerostatics node 14, wherein, the first power plant 122 and second power plant 142 can take cross propeller layout type, in order to which aerostat is controlled vertically to transport Dynamic, propeller uses feather propeller, when pitch is negative, aerostat can be controlled to move downward.

In DATA REASONING acquisition system provided in an embodiment of the present invention, the first power plant 122 and the second power plant 142 It is only illustrated by taking cross propeller layout type as an example, to realize that DATA REASONING provided in an embodiment of the present invention obtains system Subject to, it does not limit specifically.

Embodiment 2

An embodiment of the present invention provides a kind of DATA REASONING acquisition methods.

Fig. 6 is the flow chart of DATA REASONING acquisition methods according to embodiments of the present invention.As shown in fig. 6, the present invention is implemented The DATA REASONING that a kind of DATA REASONING acquisition methods that example provides are suitable for described in the corresponding embodiments one of Fig. 1 obtains system, The DATA REASONING acquisition methods can be adapted for main aerostatics node side, and it is as follows which includes step：

Step S602, to it is any one or more from aerostatics node send control instruction, control instruction be used to indicate from The measurement position of aerostatics node and/or the measurement task for performing corresponding measurement position.

Specifically, can be adapted for main aerostatics node in DATA REASONING acquisition methods provided in an embodiment of the present invention, In, control instruction is sent to from aerostatics node after the lift-off of main aerostatics node, wherein control instruction is divided into situations below：

Situation one, when main aerostatics node rises to preset height, main aerostatics node sends survey to from aerostatics node The control instruction of position is measured, so that being moved to the measurement position in control instruction according to the control instruction from aerostatics node；

Situation two, after aerostatics node motion to measurement position, main aerostatics node is sent to from aerostatics node In the control instruction of the corresponding measurement task in measurement position, so that from aerostatics node according to the control instruction in the measurement Position performs measurement task；

Situation three, after main aerostatics node rises to preset height, main aerostatics node will include measure position and The control instruction that the measurement position performs measurement task is sent to from aerostatics node, so that from aerostatics node according to the control System instruction receives the control instruction before measurement position is moved to, and arrives at the measurement in control instruction according to the control instruction Position performs corresponding measurement task.

Wherein, be used to indicate in control instruction from aerostatics node motion to measure position location information can be comprising There is the coordinate position of longitude and latitude or measuring the three-dimensional of height or two-dimensional coordinate position, the present embodiment is to realize that DATA REASONING obtains It takes subject to method, does not limit specifically.

Step S604 is received from aerostatics node in the measurement data for measuring the measurement task that position is sent.

Specifically, according to step S602, in main aerostatics node after control instruction is sent from aerostatics node, receive from The measurement data that aerostatics node is returned according to the control instruction, wherein, which is according to control from aerostatics node Measurement position and measurement task in system instruction is by measuring obtained measurement data.

Step S606, analyzes measurement data, obtains corresponding to the measurement result of the measurement data.

Specifically, according to step S604, in main aerostatics node side, the measurement data received in step S604 is performed Processing, analysis and arrangement, and any one of following operation is performed after arrangement：

Operation one, main aerostatics node stores the measurement data after arrangement；

Operation two, the measurement data after arrangement is sent to ground control station by main aerostatics node；

Operation three, main aerostatics node stores the measurement data after the arrangement, and by the measurement data after ground is returned to Take back ground control station.

The above embodiments of the present application provide a kind of DATA REASONING acquisition methods.Control is sent using to from aerostatics node Instruction, control instruction are used to indicate from aerostatics node measurement position and/or perform the corresponding measurement task for measuring position；It connects It receives from aerostatics node in the measurement data for measuring the measurement task that position is sent；DATA REASONING is completed according to measurement data, is reached The purpose of measurement range can be changed according to measurement task by having arrived, it is achieved thereby that the technique effect of upper air wind measuring efficiency is promoted, And then solves the skill for survey demeanour being caused to enclose measurement range that is small and then limiting upper air wind measuring due to the fixation of surface-based observing station Art problem.

Specifically, the step S602 to S606 that the above embodiments of the present application are provided can be shown in Fig. 1 DATA REASONING Run in acquisition system, due to setting main aerostatics node and multiple from aerostatics node, main aerostatics node and it is multiple from After the lift-off of aerostatics node, the Aerial parts in DATA REASONING acquisition system, main aerostatics node can be used as entire aerial The center (or center of circle) of measurement, is dispersed in from aerostatics node around main aerostatics node, using main aerostatics node as circle For the heart, using main aerostatics node as the center of circle, the predeterminated position stored according to main aerostatics intra-node rises to preset height, And control instruction, order are sent from the position arrived at needed for aerostatics node to from aerostatics node according to pre-stored control From aerostatics node using main aerostatics node as the center of circle, pre-determined distance for radius arrive at needed for the position arrived at, and from floating Device node performs measurement task after arriving at the position, by this setting ground control station can obtain main aerostatics node and from The measurement range and measurement data of aerostatics node, and since DATA REASONING obtains the main aerostatics node of Aerial parts of system It can be reduced according to the needs of measurement task or expand measured zone, that is, controlled from aerostatics node foundation measurement task not Together, it reduces or expands measured zone so that measurement range is more flexible, and can expand aerological measurement on the basis of the relevant technologies Measurement range, and then solve due to the fixation of surface-based observing station cause survey demeanour enclose survey that is small and then limiting upper air wind measuring The technical issues of measuring range.

Compared to the method for existing aerological measurement, scheme that the application provides has and improves the prior art and can not expand high-altitude The measurement range of measurement improves the technological merit of upper air wind measuring range.

Preferably, in step S602 before any one or more transmission control instructions from aerostatics node, the present invention The DATA REASONING acquisition methods that embodiment provides can also include：

Step S599 rises to elemental height according to preset configuration.

Wherein, preset configuration includes at least one of：Flight path, elemental height, survey demeanour enclose, flight path include longitude and latitude and Time point sequence surveys demeanour and encloses to determine from the measurement position of aerostatics node.

Specifically, main aerostatics node rises to elemental height according to being pre-configured in the embodiment of the present invention, wherein, it presets Configuration is included in entire measurement task, the flight path (that is, ship trajectory) of the flight of main aerostatics node, in main aerostatics node Survey demeanour on the flight path of flight is enclosed, i.e., main aerostatics node is needed from the measurement position residing for aerostatics node.Wherein, this hair The flight path that bright embodiment provides includes longitude and latitude and time point sequence, since main aerostatics node is performing measurement task When, practical flight path also needs the height parameter of corresponding each longitude and latitude in addition to longitude and latitude, i.e. flight path should be three-dimensional coordinate, the present invention Embodiment preferably with longitude and latitude as reference, be subject to and realize DATA REASONING acquisition methods, do not limit specifically.

In addition, time point sequence is corresponding with the longitude and latitude in flight path, it is also corresponding with the measurement position from aerostatics node, That is, time point sequence is used to indicate main aerostatics node upper corresponding measurement position at every point of time, it is specific as shown in table 1：

Table 1：

Wherein, table 1 is the position coordinates of the main aerostatics node of corresponding Each point in time and is sat from the position of aerostatics node Mark, be used to indicate main aerostatics node with from aerostatics node in different time points fixed point detection and dynamic detection.

There may also be in a period of time, main aerostatics node location coordinate is constant, from aerostatics section for corresponding table 1 There are at least one position coordinates for point, that is, fixed point detection, constantly by expanding detection zone from aerostatics node.

Step S600, receives the first communication request sent from aerostatics node, the first communication request be used for from floating Device node establishes the first communication link.

Step S601 leads to according to the first communication request foundation from aerostatics node and from first between aerostatics node Believe link, the first communication link is used for from aerostatics node-node transmission control instruction.

Specifically, with reference to slave the first communication request of aerostatics node that step S600 is received, main aerostatics node with from The first communication link is established between aerostatics node, wherein, which is used to control to from aerostatics node-node transmission It instructs, the structure of the main aerostatics node in corresponding diagram 1 in DATA REASONING acquisition system, first communication request and control instruction It is sended and received by the first communication device 1231 in the first communication terminal 123.

Based on the preset configuration provided in above-described embodiment, to from aerostatics in step S602 provided in an embodiment of the present invention The step of node transmission control instruction, can include：

Step A generates control instruction according to preset configuration, and control instruction is used to indicate from the measurement position of aerostatics node It puts and/or the corresponding measurement task for measuring position, measurement task includes at least one of：Measuring wind speed, ground mapping, boat Sky shooting, weather forecast；

Specifically, corresponding DATA REASONING shown in FIG. 1 obtains system, control instruction is generated by the first computer 121, the One computer 121, will be from the measurement position in the high-altitude that aerostatics node will arrive at and the corresponding measurement according to preset configuration The measurement task that position performs carries out packing encapsulation, generates control instruction.

Wherein, the control instruction of generation includes situations below：

Situation one generates control instruction according to from the measurement position of aerostatics node；

That is, main aerostatics node generation carries the control instruction of measurement position arrived at from aerostatics node needs.

Situation two generates control instruction according to from the measurement task of aerostatics node；

That is, main aerostatics node generation carries the control instruction of measurement task performed from aerostatics node needs.

Situation three generates control instruction according to from the measurement position of aerostatics node and measurement task；

That is, main aerostatics node generation carries the control instruction from aerostatics node measurement position and measurement task.

Above-mentioned three kinds of situations generate three kinds of situations of control instruction for main aerostatics node, that is, main aerostatics node can be with It selects at least to carry any one following information in the control instruction of generation：Information 1 measures position；Information 2, measurement task；Letter Breath 3 measures position and measurement task.For 2 two kinds of information 1 and information, due to as control instruction elder generation photos and sending messages 1 and information 2 In it is arbitrary in a completion for all not interfering with entire measurement task because information 1 and information 2 are being sent to from aerostatics section After point, if main aerostatics node receives the confirmation feedback from aerostatics node, the corresponding part lacked, example can be sent Such as, it is assumed that only carried in the control instruction of main aerostatics node generation and measure position, receiving the confirmation from aerostatics node The measurement task of the corresponding measurement position can be sent to after feedback from aerostatics node；Therefore above- mentioned information 1 and information 2 It can be separately as one kind in control instruction type.

Step B sends control instruction by the first communication link to from aerostatics node.

Specifically, main aerostatics node is by the first communication device 1231 in the first communication terminal 123, it is logical via first The control instruction that letter chain road direction is generated from aerostatics node forwarding step A.

In addition, except the type of above-mentioned control instruction, main aerostatics node can be according in the first communication request received What is carried is current from the position of aerostatics node, the position coordinates being presently in from aerostatics node is corrected, process can With as follows：

Step1. the first communication request is received；

Step2. the first communication request is parsed, is obtained from the current position coordinates of aerostatics node；

Step3. the position coordinates current according to this, with pre-stored from the position coordinates arrived at needed for aerostatics node It is compared, generation is used for the control instruction of correction；

Step4. the control instruction is sent to from aerostatics node；

Wherein, correction instruction is sent to from aerostatics by the first communication device 1231 in the first communication terminal 123 Node.

Step5. the confirmation feedback from aerostatics node is received.

From the foregoing, it will be observed that the process of Step1 to Step5 corrects the mistake from aerostatics node location coordinate for main aerostatics node Journey, by the transmission correction of control instruction from the position coordinates of aerostatics node, control instruction provided in an embodiment of the present invention, with It realizes subject to DATA REASONING acquisition methods, does not limit specifically.

In addition, main aerostatics node and from sending test between aerostatics node on the first communication link by periodicity Instruction, determines main aerostatics node and from the connection status between aerostatics node, to ensure first, from aerostatics node in master In the control range of aerostatics node；Second, the first communication link between aerostatics node and main aerostatics node is kept It is unobstructed.

Preferably, it is received in step S604 from aerostatics node in the measurement number for measuring the correspondence measurement task that position is sent According to before, DATA REASONING acquisition methods provided in an embodiment of the present invention can also include：

Step S603, receives the second communication request sent from aerostatics node, the second communication request be used for from floating Device node establishes the second communication link；

Step S605 leads to according to the second communication request foundation from aerostatics node and from second between aerostatics node Believe link, the measurement data that the second communication link sends for reception from aerostatics node；

Specifically, with reference to slave the second communication request of aerostatics node that step S603 is received, main aerostatics node with from The second communication link is established between aerostatics node, wherein, which is used to control to from aerostatics node-node transmission It instructs, the structure of the main aerostatics node in corresponding diagram 1 in DATA REASONING acquisition system, second communication request and measurement data It is received by the secondary communication device 1232 in the first communication terminal 123.

Based on the second communication link provided in above-described embodiment, in step S604 provided in an embodiment of the present invention receive from Aerostatics node can include in the step of measurement data for measuring the correspondence measurement task that position is sent：

It is received by the second communication link according to predetermined period from aerostatics node in the measurement data for measuring position.

Specifically, main aerostatics node is between aerostatics node on the basis of the second communication link is established, from When aerostatics node performs measurement task, main aerostatics node receives the corresponding survey sent from aerostatics node according to predetermined period Measure the measurement data of position.

Based on the DATA REASONING acquisition methods that the embodiments of the present invention provide, one of in the following manner, step S606, The step of analyzing measurement data, obtaining the measurement result of corresponding measurement data includes any one following embodiment：

Mode one stores measurement data；

Specifically, DATA REASONING acquisition methods provided in an embodiment of the present invention, system is obtained with reference to DATA REASONING shown in FIG. 1 System in order to ensure the normal operation of the first computer 121 in main aerostatics node, reduces the calculation amount of the first computer 121, can First to store the measurement data that the slave aerostatics node received is sent, when ground is returned to after the completion of measurement task Ground control station is taken back by survey crew and carries out data preparation, is analyzed, processing.

Mode two, earthward tracking telemetry and command station transmission third communication request, the third communication ask to establish with ground control station Third communication link；

By the third communication link after foundation, earthward tracking telemetry and command station sends measurement data.

Specifically, DATA REASONING acquisition methods provided in an embodiment of the present invention, system is obtained with reference to DATA REASONING shown in FIG. 1 System, in order to ensure that ground control station can be main floating in time to being arranged, analyzing, handling from the measurement data of aerostatics node Third communication link is established between pocket node and ground control station, receives from aerostatics node and sends in main aerostatics node Measurement data after, ground control station is just sent to by third communication link, wherein, main aerostatics node pass through first communication Measurement data via third communication link, is sent to ground control station by the secondary communication device 1232 in terminal 123.

DATA REASONING acquisition methods provided in an embodiment of the present invention, based on above-mentioned steps S602 to step S606, with reference to Fig. 1 Shown DATA REASONING obtains system, provides following measurement scheme：

First kind measurement scheme：One-point measurement

1st, in ground, the flight path (longitude and latitude, time point sequence) that main aerostatics node loads have been planned, elemental height, survey Demeanour is enclosed (position from aerostatics node relative to main aerostatics node)；

2nd, on ground, from aerostatics node loads elemental height, from aerostatics node elemental height and main aerostatics node Elemental height is identical；

3rd, it first lets main aerostatics node fly away, leads in main high-altitude aerostatics node when fixed point height is berthed with ground control station It crosses to establish according to star terminal and connect, then let fly away successively from aerostatics node；

4th, during each elemental height specified from the arrival of aerostatics node, actively pass through with main aerostatics node according to star end Connection is established at end；

5th, main aerostatics node by according to star terminal to from aerostatics node send control instruction, wherein, the control instruction Including making the location information from aerostatics node motion to precalculated position；

6th, the second power plant is adjusted, physical location is made (to be set by GPS by corresponding control algolithm from aerostatics node It is standby to obtain) and control instruction (from aerostatics node location) in step 5 deviation in a certain range；

7th, after adjusting the second power plant, shape, control computer are moved with the wind from aerostatics node into unpowered At a certain time interval, reading speed and position from GPS device, and save it in and calculated from aerostatics node control In the storage medium of machine；

8th, after the requirement from aerostatics node by receiving main aerostatics node requests data according to star terminal, then establish with The data such as position, speed, time point in a upper period are transmitted to main aerostatics node by the L-band connection of main aerostatics node, Measurement data is stored in the storage medium of the first computer of main aerostatics node by main aerostatics node；

9th, at the end of surveying wind process, ground control station sends recovery command (specified recovery point position to main aerostatics node It puts)；

10th, main aerostatics node is under the control of the first computer, in addition to the first power plant is adjusted, while to from floating Device node sends landing recovery command, so that being recycled from aerostatics node and the landing of main aerostatics node；

11st, processing is solved respectively from the corresponding data (position, speed, time point) in aerostatics node by data processing Calculate the entire wind speed for surveying wind region.

Second class measurement scheme：Dynamic measures

1st, ground control station sends main aerostatics node motion instruction (comprising mobile aiming spot)；

2nd, for main aerostatics node under the control of the first computer, the first power plant of adjustment is moved to corresponding position；

3rd, main aerostatics node is calculated from the expectation target position of aerostatics node；

4th, main aerostatics node to from aerostatics node transmission will be from aerostatics node motion to the shifting of expectation target position Dynamic instruction；

5th, with the step 6 in first kind measurement scheme.

The embodiment of the present invention automates high-altitude wind measurement, intelligent, round-the-clock, on a large scale, and changes by load After dress, different types of Distributed probing and measurement task can be realized.

The embodiment of the present invention is communicated using principal and subordinate's aerostatics node, between aerostatics node and ground control station Mode, by main aerostatics node to from aerostatics node carry out Control ＆ data acquisition, can realize high-altitude wind measurement from Dynamicization, it is intelligent, and since main aerostatics node can set offline flight path, therefore can realize large-scale high-altitude wind measurement, Due to carrying out locating and tracking to it using GPS, therefore it can realize that round-the-clock high air measures, without by meteorological conditions such as hazes Influence.And due to the design using flexibility, load certain modification is then adapted to different types of task.

Embodiment 3

Fig. 7 is the flow chart of DATA REASONING acquisition methods according to embodiments of the present invention.As shown in fig. 7, the present invention is implemented The DATA REASONING that a kind of DATA REASONING acquisition methods that example provides are suitable for described in the corresponding embodiments one of Fig. 1 obtains system, The DATA REASONING acquisition methods can be adapted for from aerostatics node side, and it is as follows which includes step：

Step S702, receives the control instruction that main aerostatics node is sent, control instruction be used to indicate measure position and/ Or perform the corresponding measurement task for measuring position.

Specifically, can be adapted in DATA REASONING acquisition methods provided in an embodiment of the present invention from aerostatics node, In, after the lift-off of aerostatics node, when being arrived at from aerostatics node with main aerostatics node sustained height, receive main floating Device node sends control instruction, and wherein control instruction is divided into situations below：

Situation one when being arrived at from aerostatics node with main aerostatics node sustained height, is received from aerostatics node and is led Aerostatics node sends the control instruction for measuring position, refers to so that being moved to control according to the control instruction from aerostatics node Measurement position in order；

Situation two after measurement position is risen to from aerostatics node, receives main aerostatics node and is sent in the measurement position The control instruction of corresponding measurement task, so that performing measurement in the measurement position from aerostatics node according to the control instruction Task；

Situation three receives from aerostatics node and measures position and in the measurement position including for main aerostatics node transmission Perform measurement task control instruction so that from aerostatics node according to the control instruction be moved to measure position before receive Corresponding measurement task is performed to the control instruction, and according to the measurement position that the control instruction is arrived in control instruction.

Step S704 is performed according to the position that measures in control instruction in the measurement task for measuring position；

Specifically, according to step S702, after the control instruction for receiving that main aerostatics node is sent from aerostatics node, according to The measurement data of corresponding measurement task is fed back according to the control instruction, wherein, which is according to control from aerostatics node Measurement position and measurement task in system instruction is by measuring obtained measurement data.

Step S706, to the measurement data of main aerostatics node return measurement task.

Specifically, according to step S704, after control instruction is received from aerostatics node, measurement task is performed, will be surveyed The corresponding measurement data of amount task beams back main aerostatics node.

The above embodiments of the present application provide a kind of DATA REASONING acquisition methods.It is sent using the main aerostatics node of reception Control instruction, control instruction are used to indicate the measurement task for measuring position and/or performing corresponding measurement position.Refer to according to control The position that measures in order is performed in the measurement task for measuring position.The measurement data of measurement task is sent to main aerostatics node. Achieve the purpose that measurement range can be changed automatically according to measurement task, it is achieved thereby that promoting the technology of upper air wind measuring efficiency Effect, and then solve since the fixation of surface-based observing station causes survey demeanour to enclose measurement range that is small and then limiting upper air wind measuring The technical issues of.

Preferably, before the control instruction for receiving that main aerostatics node is sent in step S702, the embodiment of the present invention provides DATA REASONING acquisition methods can also include：

Step S701 sends the first communication request to main aerostatics node, and the first communication request is used for and main aerostatics section Point establishes the first communication link.

Specifically, from aerostatics node rise to after main aerostatics node sustained height, from aerostatics node to master Aerostatics node sends the first communication request, so that main aerostatics node is after first communication request is received, main floating Device node and from establishing the first communication link between aerostatics node, wherein, pass through first communication link from aerostatics node Receive the control instruction that main aerostatics node is sent, the knot of the slave aerostatics node in corresponding diagram 1 in DATA REASONING acquisition system Structure, first communication request are sent by the third communication device 1431 in the second communication terminal 143.

Preferably, the step of control instruction that main aerostatics node is sent is received in step S702 can include：

The control instruction of main aerostatics node transmission is received by the first communication link, control instruction, which is used to indicate, measures position It puts and/or the corresponding measurement task for measuring position, measurement task includes at least one of：Measuring wind speed, ground mapping, boat Sky shooting, weather forecast.

Specifically, the structure of the slave aerostatics node of system is obtained with reference to DATA REASONING shown in FIG. 1, from aerostatics node The control instruction that main aerostatics node sent by the first communication link is received by third communication device 1431.

Preferably, in step S706 before the measurement data of main aerostatics node return measurement task, the present invention is real Applying the DATA REASONING acquisition methods of offer can also include：

Step S705 sends the second communication request to main aerostatics node, and the second communication request is used for and main aerostatics section Point establishes the second communication link.

Specifically, from aerostatics node after control instruction is received, in order to refer to from aerostatics node in reception control The measurement data of the measurement task performed after order passes main aerostatics node back, since the data volume of measurement data compares control instruction It is very high to the instruction of communication link requirement, so in order to ensure be not take up between aerostatics node and main aerostatics node the One communication link, from aerostatics node to main aerostatics node send the second communication request, for establish main aerostatics node with From the second communication link for data transfer between aerostatics node.

Based on the DATA REASONING acquisition methods that the embodiments of the present invention provide, returned in step S706 to main aerostatics node The step of measurement data for returning measurement task, can include：

By the second communication link according to measurement data from predetermined period to main aerostatics node return measurement position.

Specifically, on the basis of aerostatics node establishes the second communication link between main aerostatics node, from After aerostatics node performs measurement task, each the corresponding survey of each measurement position is sent from aerostatics node according to predetermined period The corresponding measurement data of amount task.

To sum up, the DATA REASONING for system and Fig. 6 and Fig. 7 offers being obtained with reference to the DATA REASONING that Fig. 1 to Fig. 5 is provided obtains Method is taken, when performing the DATA REASONING task for surveying wind, main aerostatics node 12 is after scheduled measurement position is arrived in lift-off, Xiang Cong Aerostatics node 14 sends control instruction, is specified so that being moved in control instruction by current position from aerostatics node 14 Measurement position, from aerostatics node 14 arrive at measure position after, from aerostatics node 14 according to the measurement in control instruction Task surveys wind task, the wind speed of air position A, wind direction, humidity, temperature, air pressure etc. that are presently in are surveyed wind task and carried out It measures, the measurement data at air position A is further fed back into main aerostatics node 12, by main aerostatics node 12 to this Measurement data, which is stored, arranged or first stored to carry out arranging again, finally takes back ground control station；If in addition, main aerostatics node 12 need expand measurement range, can by from aerostatics node send control instruction, by from aerostatics node by current Air position A is moved to air position B so that after expansion ranging from：Using main aerostatics node 12 be presently in position as The center of circle, using by main aerostatics node 12 be presently in position to air position B distance X km as radius circular trace region, The circular trace region is performed and surveys wind task.

It wherein, then can be with main floating when the slave aerostatics node 14 in DATA REASONING acquisition system is multiple nodes Centered on device node 12 (or, center of circle), with the mobile change measurement range of main aerostatics node 12, and can also be according to main The control instruction of aerostatics node 12 expands or shrinks measurement range so that more for variable and real on measurement task is performed Effect property (that is, the measurement range according to practical measurement task performs measurement task to measured zone in real time).

The DATA REASONING acquisition methods that the embodiment of the present invention 2 and embodiment 3 are provided, stand respectively in main aerostatics node and DATA REASONING acquisition methods are expounded from the angle of aerostatics node, wherein, embodiment 2 is built upon with embodiment 3 In embodiment 1 on the basis of DATA REASONING acquisition system shown in FIG. 1, in actually measuring, in addition to wind task is surveyed, the application reality The measurement tasks such as ground mapping, Aerial photography, weather forecast can also be performed in the DATA REASONING acquisition system for applying example offer, In, main aerostatics node can be according to the difference of measurement task, and carrying is multiple from aerostatics node, and one is formed in high-altitude with this Network is measured, ground control station can be sent to main aerostatics node by the communication link between main aerostatics node and be operated Instruction so that main aerostatics node control expands or shrinks measurement range from aerostatics node, and by main aerostatics node, Communication link between aerostatics node and ground control station can realize measurement data regional measured by obtaining in time, And measurement range can be expanded according to measurement task, more efficient measuring method is provided for aerological measurement.

It should be noted that for aforementioned each method embodiment, in order to be briefly described, therefore it is all expressed as a series of Combination of actions, but those skilled in the art should know, the present invention is not limited by described sequence of movement because According to the present invention, certain steps may be used other sequences or be carried out at the same time.Secondly, those skilled in the art should also know It knows, embodiment described in this description belongs to preferred embodiment, and involved action and module are not necessarily of the invention It is necessary.

Through the above description of the embodiments, those skilled in the art can be understood that according to above-mentioned implementation The method of example can add the mode of required general hardware platform to realize by software, naturally it is also possible to by hardware, but it is very much In the case of the former be more preferably embodiment.Based on such understanding, technical scheme of the present invention is substantially in other words to existing The part that technology contributes can be embodied in the form of software product, which is stored in a storage In medium (such as ROM/RAM, magnetic disc, CD), used including some instructions so that a station terminal equipment (can be mobile phone, calculate Machine, server or network equipment etc.) perform method described in each embodiment of the present invention.

Embodiment 4

According to embodiments of the present invention, a kind of device embodiment for being used to implement the above method is additionally provided, the application is above-mentioned The device that embodiment is provided can be run on main aerostatics node.

Fig. 8 is the structure diagram of according to embodiments of the present invention two DATA REASONING acquisition device.

As shown in figure 8, in main aerostatics node side, which can include：Sending module 82, first Receiving module 84 and measurement module 86, wherein,

Sending module 82, for sending control instruction from aerostatics node to any one or more, control instruction is used for It indicates from the measurement position of aerostatics node and/or performs the corresponding measurement task for measuring position；

First receiving module 84, for receiving from aerostatics node in the measurement number for measuring the measurement task that position is sent According to；

Measurement module 86 is electrically connected communication connection, for being connect to the first receiving module 84 with the foundation of the first receiving module 84 The measurement data received is analyzed, and obtains corresponding to the measurement result of the measurement data.

Specifically, by the corresponding main aerostatics nodes 12 of Fig. 2 it is found that be carried through this embodiment in main aerostatics node side The data acquisition facility of confession realizes data capture method, main aerostatics in 82 and first receiving module of sending module, 84 corresponding diagram 2 First communication terminal 123 in node 12, the first calculator 121 in main aerostatics node 12 in 86 corresponding diagram 2 of measurement module.

Preferably, Fig. 9 is a kind of structure diagram of according to embodiments of the present invention two DATA REASONING acquisition device, is such as schemed Shown in 9, which further includes：Power plant module 79, the second receiving module 80 and the first link establishment module 81, Wherein,

Power plant module 79, for it is any one or more send control instructions from aerostatics node before, according to default Configuration rises to elemental height；

Second receiving module 80, for receiving the first communication request sent from aerostatics node, the first communication request is used In with establishing the first communication link from aerostatics node；

First link establishment module 81 is established with the second receiving module 80 and is communicated to connect, for according to the second receiving module First communication request of the 80 slave aerostatics nodes received is established and is led to from the first communication link between aerostatics node, first Believe that link is used for from aerostatics node-node transmission control instruction；

Specifically, realize data recipient for the data acquisition facility provided through this embodiment in main aerostatics node side Method, the first power plant 122, the first aerostatics 124 and in the 2 main aerostatics node 12 of function corresponding diagram of power plant module 79 One carrier 12 5；In the function corresponding diagram 2 of second receiving module 80 and the first link establishment module 81 in main aerostatics node 12 One communication terminal 123.

Based on the DATA REASONING acquisition device that above-described embodiment provides, Figure 10 is according to embodiments of the present invention two another kind The structure diagram of DATA REASONING acquisition device, as shown in Figure 10, sending module 82, including：Instruction generation unit 821 and instruction Transmitting element 822, wherein,

Instruction generation unit 821, for generating control instruction according to preset configuration, control instruction is used to indicate from aerostatics The measurement position of node and/or the corresponding measurement task for measuring position, measurement task include at least one of：Measuring wind speed, Ground mapping, Aerial photography, weather forecast；

Instruction sending unit 822, with instruction generation unit 821 establish communicate to connect, for pass through the first communication link to The control instruction of the generation of instruction generation unit 821 is sent from aerostatics node.

Specifically, the first computer 121 in the function corresponding diagram 2 of instruction generation unit 821 in main aerostatics node 12, First communication device in the function corresponding diagram 3 of instruction sending unit 822 in main aerostatics node 12 in first communication terminal 123 1231。

Preferably, Figure 11 is the structure diagram of according to embodiments of the present invention two another DATA REASONING acquisition device, As shown in figure 11, which further includes：83 and second link establishment module 85 of third receiving module, wherein,

Third receiving module 83, for receiving from aerostatics node in the survey for measuring the correspondence measurement task that position is sent Before measuring data, receive the second communication request sent from aerostatics node, the second communication request for from aerostatics node Establish the second communication link；

Second link establishment module 85 is established with third receiving module 83 and is communicated to connect, for according to third receiving module Second communication request of the 83 slave aerostatics nodes received is established and is led to from the second communication link between aerostatics node, second The measurement data that letter link sends for reception from aerostatics node.

Preferably, Figure 12 is the structure diagram of according to embodiments of the present invention two another DATA REASONING acquisition device, As shown in figure 12, the first receiving module 84, including：

Receiving unit 841 is received from aerostatics node according to predetermined period in measurement position for passing through the second communication link The measurement data put.

Specifically, the function corresponding diagram 3 of third receiving module 83, the second link establishment module 85 and the first receiving module 84 Secondary communication device 1232 in middle main aerostatics node 12 in first communication terminal 123.

Preferably, Figure 13 is the structure diagram of according to embodiments of the present invention two another DATA REASONING acquisition device, As shown in figure 13, measurement module 86, including：Storage unit 861, request transmitting unit 862 and data transmission unit 863, wherein,

Storage unit 861, for storing measurement data；Alternatively,

Request transmitting unit 862, for earthward tracking telemetry and command station send the third communication request, the third communication request for ground Face tracking telemetry and command station establishes third communication link；

Data transmission unit 863, for passing through the third communication link after establishing, earthward tracking telemetry and command station sends measurement data.

Specifically, first computer 121, request are sent out in main aerostatics node 12 in the function corresponding diagram 2 of storage unit 861 Send in the function corresponding diagram 2 of unit 862 and data transmission unit 863 first communication terminal 123 in main aerostatics node 12.

Embodiment 5

According to embodiments of the present invention, a kind of device embodiment for being used to implement the above method is additionally provided, the application is above-mentioned The device that embodiment is provided can be run from aerostatics node.

Figure 14 is the structure diagram of according to embodiments of the present invention three DATA REASONING acquisition device.

As shown in figure 14, from aerostatics node side, which can include：Command reception module 1402nd, measurement module 1404 and data transmission blocks 1406, wherein,

Command reception module 1402, for receiving the control instruction that main aerostatics node is sent, control instruction is used to indicate It measures position and/or performs the corresponding measurement task for measuring position；

Measurement module 1404 is established with command reception module 1402 and is communicated to connect, for according to the measurement in control instruction Position is performed in the measurement task for measuring position；

Data transmission blocks 1406, for the measurement data of main aerostatics node return measurement task.

It is specifically, corresponding from aerostatics node 14 it is found that be carried through this embodiment from aerostatics node side by Fig. 4 The data acquisition facility of confession realizes the function correspondence of data capture method, command reception module 1402 and data transmission blocks 1406 From the second communication terminal 143 in aerostatics node 14, the function correspondence of measurement module 1404 is from aerostatics node 14 Two computers 141.

Preferably, Figure 15 is a kind of structure diagram of according to embodiments of the present invention three DATA REASONING acquisition device, such as Shown in Figure 15, which further includes：

Sending module 1401, for before receiving the control instruction that main aerostatics node is sent, being sent out to main aerostatics node The first communication request is sent, the first communication request is used to establish the first communication link with main aerostatics node.

Based on the DATA REASONING acquisition device that above-described embodiment provides, Figure 16 is according to embodiments of the present invention three another kind The structure diagram of DATA REASONING acquisition device, as shown in figure 16, command reception module 1402, including：

Instruction reception unit 14021, for passing through the control instruction that the first communication link receives main aerostatics node and sends, Control instruction, which is used to indicate, measures position and/or the corresponding measurement task for measuring position, measurement task include it is following at least it One：Measuring wind speed, ground mapping, Aerial photography, weather forecast.

Specifically, the function corresponding diagram of the command reception module 1402 in sending module 1401 and command reception module 1402 Third communication device 1431 in 5 from aerostatics node 14 in second communication terminal 143.

Preferably, Figure 17 is the structure diagram of according to embodiments of the present invention three another DATA REASONING acquisition device, As shown in figure 17, which further includes：

Request sending module 1405, for before the measurement data to main aerostatics node return measurement task, to master Aerostatics node sends the second communication request, and the second communication request is used to establish the second communication link with main aerostatics node.

Based on the DATA REASONING acquisition device that above-described embodiment provides, Figure 18 is according to embodiments of the present invention three another kind The structure diagram of DATA REASONING acquisition device, as shown in figure 18, data transmission blocks 1406, including：

Data transmission unit 14061 returns for passing through the second communication link according to predetermined period to main aerostatics node Measure the measurement data of position.

Specifically, the function of the data transmission unit 14061 in request sending module 1405 and data transmission blocks 1406 Fourth communication device 1432 in corresponding diagram 5 from aerostatics node 14 in second communication terminal 143.

One of ordinary skill in the art will appreciate that all or part of step in the various methods of above-described embodiment is can To be completed by program come command terminal device-dependent hardware, which can be stored in a computer readable storage medium In, storage medium can include：Flash disk, read-only memory (Read-Only Memory, ROM), random access device (Random Access Memory, RAM), disk or CD etc..

Claims

1. a kind of DATA REASONING obtains system, which is characterized in that including：

Main aerostatics node, from aerostatics node and ground control station, wherein,

The main aerostatics node is communicated to connect with multiple described established from aerostatics node, the multiple from floating for controlling Device node motion obtains to corresponding measurement position and analyzes the multiple measurement from aerostatics node in the measurement position Data；

The ground control station is established with the main aerostatics node and is communicated to connect, and the main aerostatics node is controlled for passing through Instruction is described to perform measurement task from aerostatics node；

Wherein, the measurement task includes at least one of：Measuring wind speed, ground mapping, Aerial photography, weather forecast；

After the main aerostatics node and the lift-off from aerostatics node, the main aerostatics node is entire DATA REASONING The control centre of acquisition system, wherein, the main aerostatics nodal function includes three aspects, and first aspect is from floating with described Device node communicates, and obtains the velocity information from the current location of aerostatics node and corresponding current location；Second party Face is in executive control operation, and control instruction is sent from aerostatics node to described；The third aspect is that acquisition is described from floating The response message for the destination locations that device node is set after control instruction is received in control instruction is arrived at and the arrival purpose position The headway data put；It is the execution system that DATA REASONING obtains system by multiple test clusters formed from aerostatics node System, flight position, the corresponding speed of the position and time point data during including acquiring without control flight, and periodically floated with the master Pocket node establishes the antenna transmission link of antenna L frequency ranges, by current location, the speed of corresponding current location, time point data Pass through L frequency range wireless transmissions to the main aerostatics node.

2. DATA REASONING according to claim 1 obtains system, which is characterized in that the main aerostatics node includes：The One computer, the first power plant, the first communication terminal, the first aerostatics and first vector, wherein,

The first vector is used to carry first computer, first power plant and first communication terminal；

First computer establishes communication connection respectively with first power plant and first communication terminal, for leading to It crosses and first power plant is controlled to rise to preset height or determining current air position, by controlling first communication eventually End and the ground control station described communicate, and store the measurement from the transmission of aerostatics node from aerostatics node Data；

First aerostatics is connect with the first vector, for providing aerostatic buoyancy for the first vector.

3. DATA REASONING according to claim 2 obtains system, which is characterized in that first power plant is propeller Structural dynamic device.

4. DATA REASONING according to claim 2 obtains system, which is characterized in that first communication terminal includes：The One communication device and secondary communication device, wherein,

The first communication device is used for any one or more described from aerostatics node transmission control instruction；

The secondary communication device is used to receive any one or more measurement data returned from aerostatics node.

5. DATA REASONING according to claim 1 obtains system, which is characterized in that described to include from aerostatics node：The Two computers, the second power plant, the second communication terminal, the second aerostatics and Second support, wherein,

The Second support is used to carry the second computer, second power plant and second communication terminal；

The second computer is established with second power plant and second communication terminal and is communicated to connect, for according to institute The control instruction of the main aerostatics node that the second communication terminal receives is stated, second power plant is controlled to reach and is corresponded to The measurement position of the control instruction, and measurement data is sent to the main aerostatics node by second communication terminal； Second aerostatics is connect with the Second support, for providing aerostatic buoyancy for the Second support.

6. DATA REASONING according to claim 5 obtains system, which is characterized in that second power plant is propeller Structural dynamic device.

7. DATA REASONING according to claim 5 obtains system, which is characterized in that second communication terminal includes：The Three communication devices and fourth communication device, wherein,

The third communication device is used to receive the control instruction that the main aerostatics node is sent；

The fourth communication device is used to return to the measurement data to the main aerostatics node.

8. a kind of DATA REASONING acquisition methods, which is characterized in that obtained applied to any DATA REASONING of claim 1 to 7 System is taken, including：

To it is any one or more it is described send control instruction from aerostatics node, the control instruction is used to indicate described from floating The measurement position of pocket node and/or the measurement task for performing the corresponding measurement position；

Receive the measurement data of the measurement task sent from aerostatics node in the measurement position；

The measurement data is analyzed, obtains corresponding to the measurement result of the measurement data；

After main aerostatics node and the lift-off from aerostatics node, the main aerostatics node is that entire DATA REASONING obtains The control centre of system, wherein, the main aerostatics nodal function includes three aspects, and first aspect is from aerostatics section with described Point communicates, and obtains the velocity information from the current location of aerostatics node and corresponding current location；Second aspect is In executive control operation, control instruction is sent from aerostatics node to described；The third aspect is that acquisition is described from aerostatics section It puts the response message of the destination locations set in control instruction is arrived at after control instruction is received and arrives at the destination locations Headway data；It is the execution system that DATA REASONING obtains system by multiple test clusters formed from aerostatics node, wraps Flight position, the corresponding speed of the position and time point data when including acquisition without control flight, and periodically with the main aerostatics Node establishes the antenna transmission link of antenna L frequency ranges, and by current location, the speed of corresponding current location, time point data passes through L Frequency range wireless transmission is to the main aerostatics node.

It is 9. according to the method described in claim 8, it is characterized in that, described to any one or more described from aerostatics node Before sending control instruction, further include：

Elemental height is risen to according to preset configuration；

First communication request sent from aerostatics node is received, first communication request is used for described from aerostatics Node establishes the first communication link；

Described the between the node from aerostatics is established according to first communication request from aerostatics node One communication link, first communication link are used for described from aerostatics node-node transmission control instruction；

Wherein, the preset configuration includes at least one of：Flight path, elemental height are surveyed demeanour and are enclosed, and the flight path includes longitude and latitude Degree and time point sequence, the survey demeanour are enclosed described from the measurement position of aerostatics node for determining.

It is 10. according to the method described in claim 9, it is characterized in that, described to any one or more described from aerostatics section The step of point transmission control instruction, includes：

The control instruction is generated according to preset configuration, the control instruction is used to indicate described from the measurement position of aerostatics node It puts and/or the corresponding measurement task for measuring position, the measurement task includes at least one of：Measuring wind speed, map Mapping, Aerial photography, weather forecast；

Control instruction is sent from aerostatics node to described by first communication link.

11. according to the method described in claim 8, it is characterized in that, from aerostatics node in the measurement described in the reception Before the measurement data for the correspondence measurement task that position is sent, further include：

Second communication request sent from aerostatics node is received, second communication request is used for described from aerostatics Node establishes the second communication link；

Described the between the node from aerostatics is established according to second communication request from aerostatics node Two communication links, second communication link are used to receive the measurement data sent from aerostatics node.

12. according to the method for claim 11, which is characterized in that from aerostatics node in the measurement described in the reception The measurement data for the correspondence measurement task that position is sent, including：

The measurement from aerostatics node in the measurement position is received according to predetermined period by second communication link Data.

13. according to the method described in claim 8, it is characterized in that, analyze the measurement data, corresponded to described in The step of measurement result of measurement data, includes any one following embodiment：

Mode one stores the measurement data；

Mode two sends third communication request to the ground control station, and the third communication asks to survey with the ground Third communication link is established at control station；

The measurement data is sent by ground control station described in the third communication chain road direction after foundation.

14. a kind of DATA REASONING acquisition methods, which is characterized in that obtained applied to any DATA REASONING of claim 1 to 7 System is taken, including：

The control instruction that the main aerostatics node is sent is received, the control instruction, which is used to indicate, to be measured position and/or perform The corresponding measurement task for measuring position；

It is performed according to the measurement position in the control instruction in the measurement task for measuring position；

The measurement data of the measurement task is returned to the main aerostatics node；

In the main aerostatics node and after the lift-off of aerostatics node, the main aerostatics node is that entire DATA REASONING obtains The control centre of system, wherein, the main aerostatics nodal function includes three aspects, and first aspect is from aerostatics section with described Point communicates, and obtains the velocity information from the current location of aerostatics node and corresponding current location；Second aspect is In executive control operation, control instruction is sent from aerostatics node to described；The third aspect is that acquisition is described from aerostatics section It puts the response message of the destination locations set in control instruction is arrived at after control instruction is received and arrives at the destination locations Headway data；It is the execution system that DATA REASONING obtains system by multiple test clusters formed from aerostatics node, wraps Flight position, the corresponding speed of the position and time point data when including acquisition without control flight, and periodically with the main aerostatics Node establishes the antenna transmission link of antenna L frequency ranges, and by current location, the speed of corresponding current location, time point data passes through L Frequency range wireless transmission is to the main aerostatics node.

15. according to the method for claim 14, which is characterized in that the control for receiving the main aerostatics node and sending Before instruction, further include：

The first communication request is sent to the main aerostatics node, first communication request is used for and the main aerostatics node Establish the first communication link.

16. according to the method for claim 15, which is characterized in that the control for receiving the main aerostatics node and sending Instruction, including：

The control instruction of the main aerostatics node transmission is received by first communication link, the control instruction is used to refer to Show that measuring position and/or the corresponding measurement task for measuring position, the measurement task includes at least one of：Wind speed Measurement, ground mapping, Aerial photography, weather forecast.

17. according to the method for claim 14, which is characterized in that described to return to the measurement to the main aerostatics node Before the measurement data of task, further include：

The second communication request is sent to the main aerostatics node, second communication request is used for and the main aerostatics node Establish the second communication link.

18. according to the method for claim 17, which is characterized in that described to return to the measurement to the main aerostatics node The measurement data of task, including：

The measurement for measuring position is returned to the main aerostatics node according to predetermined period by second communication link Data.

19. a kind of DATA REASONING acquisition device, which is characterized in that including：

Sending module, for sending control instruction from aerostatics node to any one or more, the control instruction is used to refer to Show described from the corresponding measurement task for measuring position in the measurement position of aerostatics node and/or execution；

First receiving module, for receiving the survey of the measurement task sent from aerostatics node in the measurement position Measure data；

Measurement module for analyzing the measurement data, obtains corresponding to the measurement result of the measurement data；

20. device according to claim 19, which is characterized in that described device further includes：

Power plant module, for described before any one or more transmission control instructions from aerostatics node, according to pre- establishing It puts and rises to elemental height；

Second receiving module, for receiving first communication request sent from aerostatics node, first communication request For establishing the first communication link from aerostatics node with described；

First link establishment module, for being established according to first communication request from aerostatics node with described from floating First communication link between pocket node, first communication link are used to control from aerostatics node-node transmission to described Instruction；

21. device according to claim 20, which is characterized in that the sending module, including：

Instruction generation unit, for generating the control instruction according to preset configuration, the control instruction be used to indicate it is described from The measurement position of aerostatics node and/or the corresponding measurement task for measuring position, the measurement task include it is following at least One of：Measuring wind speed, ground mapping, Aerial photography, weather forecast；

Instruction sending unit, for sending control instruction from aerostatics node to described by first communication link.

22. device according to claim 19, which is characterized in that described device further includes：

Third receiving module, in the reception correspondence measurement times sent from aerostatics node in the measurement position Before the measurement data of business, second communication request sent from aerostatics node is received, second communication request is used for With described the second communication link is established from aerostatics node；

Second link establishment module, for being established according to second communication request from aerostatics node with described from floating Second communication link between pocket node, second communication link is used to receiving described to be sent from aerostatics node Measurement data.

23. device according to claim 22, which is characterized in that first receiving module, including：

Receiving unit, for by second communication link according to predetermined period receive it is described from aerostatics node in the survey Measure the measurement data of position.

24. device according to claim 19, which is characterized in that the measurement module, including：

Storage unit, for storing the measurement data；Alternatively,

Request transmitting unit sends third communication request for earthward tracking telemetry and command station, third communication request for it is described Ground control station establishes third communication link；

Data transmission unit sends the measurement for passing through ground control station described in the third communication chain road direction after establishing Data.

25. a kind of DATA REASONING acquisition device, which is characterized in that including：

Command reception module, for receiving the control instruction that main aerostatics node is sent, the control instruction is used to indicate measurement Position and/or the measurement task for performing the corresponding measurement position；

Measurement module, for being performed according to the measurement position in the control instruction in the measurement for measuring position Task；

Data transmission blocks, for returning to the measurement data of the measurement task to the main aerostatics node；

In main aerostatics node and after the lift-off of aerostatics node, the main aerostatics node is that entire DATA REASONING obtains system Control centre, wherein, the main aerostatics nodal function include three aspect, first aspect be with it is described from aerostatics node into Row communication obtains the velocity information from the current location of aerostatics node and corresponding current location；Second aspect is to hold During row control operation, control instruction is sent from aerostatics node to described；The third aspect is to exist described in acquisition from aerostatics node It receives the response message of the destination locations set in control instruction is arrived at after control instruction and arrives at the navigation of the destination locations Speed data；It is the execution system that DATA REASONING obtains system by multiple test clusters formed from aerostatics node, including adopting Flight position, the corresponding speed of the position and time point data when collecting without control flight, and periodically with the main aerostatics node The antenna transmission link of antenna L frequency ranges is established, by current location, the speed of corresponding current location, time point data passes through L frequency ranges It is wirelessly transmitted to the main aerostatics node.

26. device according to claim 25, which is characterized in that described device further includes：

Sending module, for before receiving the control instruction that the main aerostatics node is sent, being sent out to the main aerostatics node The first communication request is sent, first communication request is used to establish the first communication link with the main aerostatics node.

27. device according to claim 26, which is characterized in that described instruction receiving module, including：

Instruction reception unit, for receiving the control instruction of the main aerostatics node transmission by first communication link, The control instruction is used to indicate the measurement task for measuring position and/or the corresponding measurement position, and the measurement task includes At least one of：Measuring wind speed, ground mapping, Aerial photography, weather forecast.

28. device according to claim 25, which is characterized in that described device further includes：

Request sending module, for before the measurement data for returning to the measurement task to the main aerostatics node, to institute It states main aerostatics node and sends the second communication request, second communication request is used to establish second with the main aerostatics node Communication link.

29. device according to claim 28, which is characterized in that the data transmission blocks, including：

Data transmission unit, for returning to institute to the main aerostatics node according to predetermined period by second communication link State the measurement data for measuring position.