CN107564340A - Unattended aircraft information gathering transmission surface process and device - Google Patents
Unattended aircraft information gathering transmission surface process and device Download PDFInfo
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- CN107564340A CN107564340A CN201710817558.2A CN201710817558A CN107564340A CN 107564340 A CN107564340 A CN 107564340A CN 201710817558 A CN201710817558 A CN 201710817558A CN 107564340 A CN107564340 A CN 107564340A
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Abstract
The invention discloses a kind of unattended aircraft information gathering transmission surface process and device, belong to airborne vehicle technical field.This method includes：The flight information that aircraft onboard Automatic dependent surveillance broadcast device is sent is obtained in real time；The real-time flight information for the airborne vehicle that radar wave detection arrives is obtained in real time；The flight information that is sent according to aircraft onboard Automatic dependent surveillance broadcast device and radar wave detection to airborne vehicle the real-time flight information of airborne vehicle that collects of real-time flight information, send control instruction to airborne vehicle.The device is implemented for this method.This method and device its can to greatest extent realize the airborne vehicle of low-latitude flying in flight range is monitored, therefore, it is possible to ensure the safety of flight environment of vehicle and airborne vehicle in itself to greatest extent.
Description
Technical field
The present invention relates to airborne vehicle technical field, is passed more particularly to a kind of unattended aircraft information gathering
Defeated surface process and device.
Background technology
In the prior art, for the general ground based navigational system used based on radar of monitoring system of airborne vehicle.But
In actual applications, the continental rise supervision equipment based on radar is due to by construction cost height, maintenance cost height and terrain shading
Etc. the influence of factor, it is difficult to realize and carry out all standing monitoring to the airborne vehicle of low-latitude flying in flight range.This is just in certain journey
The flight safety of the airborne vehicle of low-latitude flying in flight range is have impact on degree, is not only the possibility to cause safety to flight environment of vehicle
Hidden danger, also security threat can be caused in itself to airborne vehicle.
The content of the invention
In view of this, the invention provides a kind of unattended aircraft information gathering transmission surface process and dress
Put, it can to greatest extent realize and the airborne vehicle of low-latitude flying in flight range is monitored, therefore, it is possible to greatest extent
Ground ensures the safety of flight environment of vehicle and airborne vehicle in itself, thus more suitable for practicality.
In order to reach above-mentioned first purpose, unattended aircraft information gathering transmission ground provided by the invention
The technical scheme of face method is as follows：
Unattended aircraft information gathering transmission surface process provided by the invention comprises the following steps：
The flight information that aircraft onboard Automatic dependent surveillance broadcast device is sent is obtained in real time；
The real-time flight information for the airborne vehicle that radar wave detection arrives is obtained in real time；
The flight information sent according to the aircraft onboard Automatic dependent surveillance broadcast device and the radar wave are visited
The real-time flight information for the airborne vehicle that the real-time flight information of the airborne vehicle measured collects, sent to the airborne vehicle
Control instruction.
The unattended aircraft information gathering transmission surface process of present invention offer can also use following technology
Measure is further realized.
Preferably, the real-time flight information of the airborne vehicle include the airborne vehicle residing for real-time longitude and latitude, in real time
Spatial altitude, real-time flight speed and real-time aerial statue.
Preferably, the real-time flight information sent according to getting by the Automatic dependent surveillance broadcast device,
And the real-time flight information of the airborne vehicle real-time detected from the radar by radar wave is sent to the airborne vehicle
During control instruction, the control instruction includes adjusting the spatial altitude instruction of the airborne vehicle, adjusts the flight of the airborne vehicle
Speed command, the aerial statue of the adjustment airborne vehicle instruct, changed the course line instruction of the airborne vehicle, and the airborne vehicle
The danger signal alarm command in front.
Preferably, the control instruction is triggered according to real-time map.
Preferably, the real-time map includes longitude and latitude, the floor space of surface structures or vegetation, and space height
Degree.
Preferably, the real-time map also includes aviation forbidden zone markings, when the real-time flight information of the airborne vehicle
When showing that the airborne vehicle will swarm into the aviation forbidden zone markings, the mobile terminal sends the boat to the airborne vehicle
The course line instruction of pocket, forces the airborne vehicle to detour the aviation forbidden zone；Or instruction of making a return voyage is sent to the airborne vehicle, compel
The airborne vehicle is set to make a return voyage.
Preferably, on the real-time map, in the periphery of aviation forbidden zone markings, apart from the aviation forbidden zone
The position of markings setpoint distance is provided with aviation forbidden zone early warning line, when aviation described in the real-time flight presentation of information of the airborne vehicle
When device enters the aviation forbidden zone early warning line, the course line that the mobile terminal sends the airborne vehicle to the airborne vehicle instructs,
The airborne vehicle is forced to detour the aviation forbidden zone；Or instruction of making a return voyage is sent to the airborne vehicle, force the airborne vehicle to return
Boat.
Preferably, setpoint distance >=10km between aviation forbidden zone early warning line and aviation forbidden zone markings.
Preferably, the setpoint distance between aviation forbidden zone early warning line and aviation forbidden zone markings is according to
The real-time flight speed of airborne vehicle and set in real time, setting between aviation forbidden zone early warning line and aviation forbidden zone markings
The real-time flight speed v of set a distance >=airborne vehicleim/s×30s。
In order to reach above-mentioned first purpose, unattended aircraft information gathering transmission ground provided by the invention
The technical scheme of face device is as follows：
Unattended aircraft information gathering transmission ground installation provided by the invention includes airborne broadcast type certainly
Dynamic related monitoring apparatus, radar, Automatic dependent surveillance broadcast device information collecting unit, radar information collecting unit, service
Device and mobile terminal,
The airborne Automatic dependent surveillance broadcast device is loaded on the airborne vehicle, for obtaining the aviation in real time
The real-time flight information of device；
The real-time flight information that the radar passes through airborne vehicle described in radar wave real-time detection；
The Automatic dependent surveillance broadcast device information collecting unit is used to gather aircraft onboard broadcast type in real time certainly
The real-time flight information that dynamic related monitoring apparatus is sent, and the aircraft onboard Automatic dependent surveillance broadcast device that will be got
The real-time flight information real-time Transmission of transmission is to the server；
The radar information collecting unit is used to gather the airborne vehicle real-time flight information arrived by radar wave detection in real time,
And by the real-time flight information real-time Transmission of the airborne vehicle arrived by radar wave detection got to the server；
The server be used for by from the Automatic dependent surveillance broadcast device information collecting unit obtain by described
The real-time flight information that Automatic dependent surveillance broadcast device is sent, and from radar information collecting unit acquisition by institute
State the airborne vehicle that radar is real-time detected by radar wave real-time flight information collect after send to the mobile terminal；
The mobile terminal is used to by what the Automatic dependent surveillance broadcast device was sent in real time be flown according to what is got
Row information, and the airborne vehicle real-time detected from the radar by radar wave real-time flight information to the aviation
Device sends control instruction.
The unattended aircraft information gathering transmission ground installation of present invention offer can also use following technology
Measure is further realized.
Preferably, the Automatic dependent surveillance broadcast device information collecting unit, radar information collecting unit kimonos
The electric supply installation of business device includes photovoltaic power generation apparatus, battery and power supply management chip,
When the Automatic dependent surveillance broadcast device information collection described enough of electric energy caused by the photovoltaic power generation apparatus is single
Member, radar information collecting unit and server are in use, battery described in the power supply management chip controls is off；
When electric energy caused by the photovoltaic power generation apparatus is not enough to adopt for the Automatic dependent surveillance broadcast device information
Collect unit, radar information collecting unit and server in use, battery described in the power supply management chip controls is in closure
State so that the difference of the Automatic dependent surveillance broadcast device information collecting unit, radar information collecting unit and server
Volume electric energy is supplied by the batteries.
The airborne vehicle note applied in unattended aircraft information gathering transmission surface process provided by the invention
The grounded receiving station for carrying Automatic dependent surveillance broadcast device is typically established at the Civil Aviation Airport control tower of no radar surveillance equipment
On, can realize centered on single control tower, be loaded with radius 180km kilometer ranges airborne vehicle record broadcast type it is automatically related
The air traffic control monitoring of the aircraft activity of monitoring arrangement, the real-time flight letter of the airborne vehicle arrived in conjunction with radar wave detection
Breath, enables to the flying activity control monitoring range to airborne vehicle more extensive, so as to ensure airborne vehicle to greatest extent
Flight safety, and avoid being carrying out high-lager building in the flight range residing for the airborne vehicle of aerial mission, tall and big plant
The safety of quilt, ground staff etc..
Brief description of the drawings
By reading the detailed description of hereafter preferred embodiment, it is various other the advantages of and benefit it is common for this area
Technical staff will be clear understanding.Accompanying drawing is only used for showing the purpose of preferred embodiment, and is not considered as to the present invention
Limitation.And in whole accompanying drawing, identical part is denoted by the same reference numerals.In the accompanying drawings：
Fig. 1 is the step of surface process is transmitted in unattended aircraft information gathering provided in an embodiment of the present invention
Flow chart；
Fig. 2 is to be related in unattended aircraft information gathering transmission surface process provided in an embodiment of the present invention
Aviation forbidden zone markings schematic diagram；
Fig. 3 is to be related in unattended aircraft information gathering transmission surface process provided in an embodiment of the present invention
Aviation forbidden zone early warning line schematic diagram；
Fig. 4 is respectively to be set in unattended aircraft information gathering transmission ground installation provided in an embodiment of the present invention
Standby connection relationship diagram；
Fig. 5 is to be related in unattended aircraft information gathering transmission ground installation provided in an embodiment of the present invention
Electric supply installation schematic diagram.
Embodiment
The present invention is to solve the problems, such as that prior art is present, there is provided a kind of unattended aircraft information gathering passes
Defeated ground installation and method, it can to greatest extent realize and the airborne vehicle of low-latitude flying in flight range is monitored, because
This, can ensure the safety of flight environment of vehicle and airborne vehicle in itself to greatest extent, thus more suitable for practicality.
Further to illustrate the present invention to reach the technological means and effect that predetermined goal of the invention is taken, below in conjunction with
Accompanying drawing and preferred embodiment, to according to unattended aircraft information gathering proposed by the present invention transmit ground installation and
Method, its embodiment, structure, feature and its effect, describe in detail as after.In the following description, a different " implementation
What example " or " embodiment " referred to is not necessarily the same embodiment.In addition, the feature, structure or feature in one or more embodiments can
Combined by any suitable form.
The terms "and/or", only a kind of incidence relation for describing affiliated partner, expression may have three kinds of passes
System, for example, A and/or B, is specifically interpreted as：A and B can be included simultaneously, can be with individualism A, can also individualism
B, can possess above-mentioned three kinds of any situations.
Referring to accompanying drawing 1, unattended aircraft information gathering transmission surface process provided by the invention include with
Lower step：
Step S1：The flight information that aircraft onboard Automatic dependent surveillance broadcast device is sent is obtained in real time；
Step S2：The real-time flight information for the airborne vehicle that radar wave detection arrives is obtained in real time；
Step S3：The flight information and radar wave detection sent according to aircraft onboard Automatic dependent surveillance broadcast device
To airborne vehicle the real-time flight information of airborne vehicle that collects of real-time flight information, send control instruction to airborne vehicle.
The boat applied in unattended aircraft information gathering transmission surface process provided in an embodiment of the present invention
The grounded receiving station of pocket record Automatic dependent surveillance broadcast device is typically established at the airliner of no radar surveillance equipment
It on the control tower of field, can realize centered on single control tower, airborne vehicle record broadcast type is loaded with radius 180km kilometer ranges certainly
The air traffic control monitoring of the aircraft activity of dynamic related monitoring apparatus, the airborne vehicle arrived in conjunction with radar wave detection it is real-time
Flight information, enable to the flying activity control monitoring range to airborne vehicle more extensive, so as to ensure boat to greatest extent
The flight safety of pocket, and avoid being carrying out high-lager building in the flight range residing for the airborne vehicle of aerial mission,
The safety of tall and big vegetation, ground staff etc..
Wherein, the real-time flight information of airborne vehicle include airborne vehicle residing for real-time longitude and latitude, real-time spatial altitude, in real time
Flying speed and real-time aerial statue.During aircraft, the fact that its is residing longitude and latitude directly corresponding to be ground
Geographical position residing for face high-lager building, the tall and big vegetation in ground, when aircraft is tall and big on ground high-lager building, ground
Space-time on longitude and latitude described in vegetation, because ground high-lager building, the tall and big vegetation in ground are three dimensions solids, it is on ground
On the basis of the longitude and latitude of face, also extend to high-altitude, once airborne vehicle is on the ground residing for ground high-lager building, the tall and big vegetation in ground
Manage position overhead and flying height be equal to or less than corresponding ground high-lager building, the tall and big vegetation in ground spatial altitude when,
Airborne vehicle is likely to collide between ground high-lager building, the tall and big vegetation in ground at any time, and this can not only give airborne vehicle
Flight safety bring fatal harm, can also cause the tall and big vegetation of ground high-lager building, ground and high with corresponding ground
The relevant property of big building, the tall and big vegetation in ground, personnel damage, and therefore, the real-time spatial altitude of airborne vehicle is to pass
One of flight information that important needs monitor；In addition, in addition to the real-time spatial altitude of airborne vehicle, airborne vehicle was flying
Cheng Zhong, real-time flight speed and real-time the aerial statue also flight safety with airborne vehicle in itself, and airborne vehicle were flying
It is possible to have very important association to injury caused by ground high-lager building, the tall and big vegetation in ground in journey, therefore, it is also desirable to
Monitor the real-time flight speed of airborne vehicle and real-time aerial statue.
Wherein, according to the real-time flight information sent by Automatic dependent surveillance broadcast device got, and by thunder
During up to the real-time flight information of the airborne vehicle real-time detected by radar wave to airborne vehicle transmission control instruction, control instruction bag
Include adjustment airborne vehicle spatial altitude instruction, adjustment airborne vehicle flying speed instruction, adjustment airborne vehicle aerial statue instruction,
Change the course line instruction of airborne vehicle, and the danger signal alarm command in front of airborne vehicle.According to the above-mentioned reality for airborne vehicle
When flight information monitor mode and monitoring importance, when the real-time flight information that monitors produces potential threat, pass through
Corresponding control instruction is the flight condition of adjustable airborne vehicle.Specifically, when airborne vehicle is for example military into aviation no-fly zone
During forbidden zone, no matter whether there is high-lager building or tall and big vegetation in the range of the longitude and latitude residing for it, be required for changing aviation
The course line of device, now just need to instruct to change the course line of airborne vehicle, now, in relevant range by the course line for changing airborne vehicle
Do not stop forces airborne vehicle to make a return voyage or detour the military affairs in the case of airport it is necessary to instruct by changing the course line of airborne vehicle
Forbidden zone, and in the case of being provided with stop airport in relevant range, the boat can also be forced by changing the course line instruction of airborne vehicle
Pocket drops to the stop airport.In the case where airborne vehicle is in non-no-fly zone, the flying height if running into airborne vehicle
Equal to or less than ground high-lager building, the tall and big vegetation in ground so that the flight course of ground aviation device is present and ground height
During the situation for the possibility that big building, the tall and big vegetation in ground are bumped against, rise can be instructed by adjusting the spatial altitude of airborne vehicle
The flying height of airborne vehicle, to reduce the possibility that it bumps against with ground pile, the tall and big vegetation in ground.In addition, lead to
The flying speed instruction of adjustment airborne vehicle is crossed, the flying speed of airborne vehicle can be adjusted.By the aerial statue for adjusting airborne vehicle
Instruction, the aerial statue of airborne vehicle can be adjusted, in this case, the course line by changing airborne vehicle instructs, adjustment aviation
Device spatial altitude instruction, adjustment airborne vehicle flying speed instruction, adjustment airborne vehicle aerial statue instruction between arrangement,
Combination, enables to the aviation operation of airborne vehicle in a safe condition.
Wherein, control instruction is triggered according to real-time map.Because ground pile, the tall and big vegetation in ground are not one
Into constant, real-time change can be occurred according to the time, therefore, when being triggered to the control instruction of airborne vehicle, it is also necessary to examine
Consider ground pile, the real-time change situation of the tall and big vegetation in ground, real-time map is that one kind can easily and efficiently be touched according to this
Send out the references object of control instruction.
Wherein, real-time map includes longitude and latitude, the floor space of surface structures or vegetation, and spatial altitude.At this
In the case of kind, real-time map can be depicted in surface structures or vegetation factor, closely related with the flight course of airborne vehicle
Factor, therefore, it is possible to application the real-time map triggering relevant control instruction.
Referring to accompanying drawing 2, real-time map also includes aviation forbidden zone markings 1, when the real-time flight presentation of information of airborne vehicle 2 is navigated
When pocket 2 will swarm into aviation forbidden zone markings, the course line that mobile terminal sends airborne vehicle 2 to airborne vehicle 2 instructs, and forces aviation
Device 2 detours aviation forbidden zone；Or instruction of making a return voyage is sent to airborne vehicle 2, force airborne vehicle 2 to make a return voyage.In this case, aviation is prohibited
Distinctive emblem line 1 can be regarded as a kind of electronic grille fence, and the electronic grille fence can prevent airborne vehicle 2 from swarming into aviation forbidden zone, so as to ensure
Do not bothered in aviation forbidden zone by the airborne vehicle 2 of correlation.
Referring to accompanying drawing 3, on real-time map, in the periphery of aviation forbidden zone markings 1, set apart from aviation forbidden zone markings
The position of distance is provided with aviation forbidden zone early warning line 3, when the real-time flight presentation of information airborne vehicle 2 of airborne vehicle 2 enters aviation forbidden zone
During early warning line, the course line that mobile terminal sends airborne vehicle 2 to airborne vehicle 2 instructs, and forces airborne vehicle 2 to detour aviation forbidden zone；Or
Instruction of making a return voyage is sent to airborne vehicle 2, forces airborne vehicle 2 to make a return voyage.It is unique only existing because the flight of airborne vehicle 2 has inertia
Aviation forbidden zone markings 1 in the case of, it is difficult to prevent the airborne vehicle 2 caused by inertia from swarming into the situation of aviation forbidden zone
Occur, and if added again in the position of the peripheral distance aviation forbidden zone markings setpoint distance of aviation forbidden zone markings 1 together
After aviation forbidden zone early warning line 3, once airborne vehicle 2 swarms into aviation forbidden zone early warning line 3, you can the course line instruction of triggering airborne vehicle 2,
Airborne vehicle 2 is forced to detour aviation forbidden zone, or the instruction of making a return voyage of triggering airborne vehicle 2, force airborne vehicle 2 to make a return voyage, it can be avoided
Airborne vehicle 2 causes the situation for swarming into aviation forbidden zone by mistake by inertia in the case where being not provided with aviation forbidden zone early warning line 3
Occur.
Wherein, setpoint distance >=10km between aviation forbidden zone early warning line 3 and aviation forbidden zone markings 1.The setpoint distance
10km be according to acceleration of the flying speed, airborne vehicle 2 of airborne vehicle 2 in moderating process in the case of, by being calculated
Ultimate range, in the distance range of the setting, airborne vehicle 2 can be from normal flight speed reduction, assuming that airborne vehicle 2 exists
From aviation forbidden zone, early warning line reduces speed now, until in the case that speed is kept to 0 during the markings of aviation forbidden zone, can obtain the maximum
Distance is setpoint distance, and in the present embodiment, the setpoint distance is 10km.
Wherein, the setpoint distance between aviation forbidden zone early warning line 3 and aviation forbidden zone markings 1 is according to the real-time of airborne vehicle 2
Flying speed and set in real time, setpoint distance >=airborne vehicle 2 between aviation forbidden zone early warning line 3 and aviation forbidden zone markings 1
Real-time flight speed vim/s×30s.In this case, viM/s × 30s maximum is expressed as when airborne vehicle 2 is from normal
, it is necessary to take 30s when flying speed is reduced to 0, and vi=v0- at, wherein, the real-time flight speed of vi- airborne vehicles 2, m/s；a-
Acceleration of the airborne vehicle 2 after aviation forbidden zone early warning line 3 is entered, m/s2；Realities of t-vi at the time of undergoing after corresponding duration t
Shi Sudu, m/s.In this case, make to be in flight course equivalent to the time for giving the driver 30s of airborne vehicle 2
Airborne vehicle 2 slow down so that airborne vehicle 2 can have enough buffer time.
Referring to accompanying drawing 4, unattended aircraft information gathering transmission ground installation provided in an embodiment of the present invention
Including airborne Automatic dependent surveillance broadcast device, radar, Automatic dependent surveillance broadcast device information collecting unit, radar letter
Cease collecting unit, server and mobile terminal.Airborne Automatic dependent surveillance broadcast device is loaded on airborne vehicle, for real-time
Obtain the real-time flight information of airborne vehicle；The real-time flight information that radar passes through radar wave real-time detection airborne vehicle；Broadcast type is certainly
Dynamic related monitoring apparatus information acquisition unit is used to gather what aircraft onboard Automatic dependent surveillance broadcast device was sent in real time
Real-time flight information, and the real-time flight information that the aircraft onboard Automatic dependent surveillance broadcast device got is sent is real
When transmit to server；Radar information collecting unit is used to gather the airborne vehicle real-time flight letter arrived by radar wave detection in real time
Breath, and by the real-time flight information real-time Transmission of the airborne vehicle arrived by radar wave detection got to server；Server
For being sent what is obtained from Automatic dependent surveillance broadcast device information collecting unit by Automatic dependent surveillance broadcast device
Real-time flight information, and from radar information collecting unit obtain the airborne vehicle real-time detected by radar by radar wave
Real-time flight information collect after send to mobile terminal；Mobile terminal is for according to getting, by broadcast type, correlation to be supervised automatically
The real-time flight information that view apparatus is sent, and the real-time flight information of the airborne vehicle real-time detected by radar by radar wave
Control instruction is sent to airborne vehicle.
The boat applied in unattended aircraft information gathering transmission ground installation provided in an embodiment of the present invention
The grounded receiving station of pocket record Automatic dependent surveillance broadcast device is typically established at the airliner of no radar surveillance equipment
It on the control tower of field, can realize centered on single control tower, airborne vehicle record broadcast type is loaded with radius 180km kilometer ranges certainly
The air traffic control monitoring of the aircraft activity of dynamic related monitoring apparatus, the airborne vehicle arrived in conjunction with radar wave detection it is real-time
Flight information, enable to the flying activity control monitoring range to airborne vehicle more extensive, so as to ensure boat to greatest extent
The flight safety of pocket, and avoid being carrying out high-lager building in the flight range residing for the airborne vehicle of aerial mission,
The safety of tall and big vegetation, ground staff etc..
Referring to accompanying drawing 5, Automatic dependent surveillance broadcast device information collecting unit, radar information collecting unit and server
Electric supply installation include photovoltaic power generation apparatus, battery and power supply management chip.When electric energy is enough caused by photovoltaic power generation apparatus
Automatic dependent surveillance broadcast device information collecting unit, radar information collecting unit and server are in use, power supply management core
Piece control battery is off；When electric energy caused by photovoltaic power generation apparatus is not enough to fill for Automatic dependent surveillance broadcast
Information acquisition unit, radar information collecting unit and server are put in use, power supply management chip controls battery is in closure
State so that the difference electricity of Automatic dependent surveillance broadcast device information collecting unit, radar information collecting unit and server
It can be supplied by batteries.In this case, Automatic dependent surveillance broadcast device information collecting unit, radar information collection
Unit, server are able to realize that two kinds of powering modes of photovoltaic and storage battery power supply are formed by the control of power supply management chip
Complementary situation.In the case of illumination abundance, photovoltaic power generation apparatus is connected in the selection of power supply management chip, passes through photovoltaic generation
Device is Automatic dependent surveillance broadcast device information collecting unit, radar information collecting unit, server power supply, except this it
Outside, when electric energy caused by photovoltaic power generation apparatus exceedes Automatic dependent surveillance broadcast device information collecting unit, radar information
Collecting unit, server electricity consumption total load when, power supply management chip also turns on photovoltaic power generation apparatus and battery so that photovoltaic
TRT can be that battery charges.Night no light or continuous rainy weather cause electric energy caused by photovoltaic power generation apparatus
It is not enough to support that Automatic dependent surveillance broadcast device information collecting unit, radar information collecting unit, the electricity consumption of server are total
During load, power supply management chip conducting battery is adopted with Automatic dependent surveillance broadcast device information collecting unit, radar information
Collect unit, server, now, the electric energy saved by battery supports that the collection of Automatic dependent surveillance broadcast device information is single
Member, radar information collecting unit, the power load of server.As can be seen here, in this case, not only in the sufficient feelings of illumination
Electric energy caused by photovoltaic power generation apparatus can be applied under condition, in the case of the illumination deficiency caused by night or continuous wet weather,
Because the electric energy of battery savings is also by caused by photovoltaic power generation apparatus, therefore, equivalent at night or continuous overcast and rainy
In the case of caused illumination deficiency, the electric energy of application is still electric energy caused by photovoltaic power generation apparatus, therefore, in such case
Under, can solve the electric power resource of other forms to greatest extent, furthermore, because energy caused by sunshine has inexpensively without dirt
The characteristics of dye, therefore, in this case, the unattended aircraft letter for enabling to the embodiment of the present invention two to provide
The cost of breath collection transmission ground installation is largely reduced.
Although preferred embodiments of the present invention have been described, but those skilled in the art once know basic creation
Property concept, then can make other change and modification to these embodiments.So appended claims be intended to be construed to include it is excellent
Select embodiment and fall into having altered and changing for the scope of the invention.
Obviously, those skilled in the art can carry out the essence of various changes and modification without departing from the present invention to the present invention
God and scope.So, if these modifications and variations of the present invention belong to the scope of the claims in the present invention and its equivalent technologies
Within, then the present invention is also intended to comprising including these changes and modification.
Claims (10)
1. a kind of unattended aircraft information gathering transmission surface process, it is characterised in that comprise the following steps：
The flight information that aircraft onboard Automatic dependent surveillance broadcast device is sent is obtained in real time；
The real-time flight information for the airborne vehicle that radar wave detection arrives is obtained in real time；
According to the aircraft onboard Automatic dependent surveillance broadcast device send flight information and the radar wave detection to
The airborne vehicle the real-time flight information of the airborne vehicle that collects of real-time flight information, send and control to the airborne vehicle
Instruction.
2. unattended aircraft information gathering transmission surface process according to claim 1, it is characterised in that
The real-time flight information of the airborne vehicle includes real-time longitude and latitude, real-time spatial altitude, the real-time flight residing for the airborne vehicle
Speed and real-time aerial statue.
3. unattended aircraft information gathering transmission surface process according to claim 1, it is characterised in that
Pass through according to the real-time flight information sent by the Automatic dependent surveillance broadcast device got, and by the radar
When the real-time flight information for the airborne vehicle that radar wave real-time detects is to airborne vehicle transmission control instruction, the control
Instruction includes adjusting the spatial altitude instruction of the airborne vehicle, adjusts the flying speed instruction of the airborne vehicle, adjusts the boat
The aerial statue instruction of pocket, the course line instruction for changing the airborne vehicle, and the danger signal early warning in front of the airborne vehicle
Instruction.
4. unattended aircraft information gathering transmission surface process according to claim 3, it is characterised in that
The control instruction is triggered according to real-time map.
5. unattended aircraft information gathering transmission surface process according to claim 4, it is characterised in that
The real-time map includes longitude and latitude, the floor space of surface structures or vegetation, and spatial altitude.
6. unattended aircraft information gathering transmission surface process according to claim 4, it is characterised in that
The real-time map also includes aviation forbidden zone markings, when airborne vehicle described in the real-time flight presentation of information of the airborne vehicle will
When swarming into the aviation forbidden zone markings, the course line that mobile terminal sends the airborne vehicle to the airborne vehicle instructs, and forces institute
Airborne vehicle is stated to detour the aviation forbidden zone；Or instruction of making a return voyage is sent to the airborne vehicle, force the airborne vehicle to make a return voyage.
7. unattended aircraft information gathering transmission surface process according to claim 6, it is characterised in that
On the real-time map, in the periphery of aviation forbidden zone markings, apart from the aviation forbidden zone markings setpoint distance
Position is provided with aviation forbidden zone early warning line, when airborne vehicle described in the real-time flight presentation of information of the airborne vehicle is prohibited into the aviation
During area's early warning line, the course line that the mobile terminal sends the airborne vehicle to the airborne vehicle instructs, force the airborne vehicle around
The row aviation forbidden zone；Or instruction of making a return voyage is sent to the airborne vehicle, force the airborne vehicle to make a return voyage.
8. unattended aircraft information gathering transmission surface process according to claim 7, it is characterised in that
Setpoint distance >=10km between aviation forbidden zone early warning line and aviation forbidden zone markings；
Preferably, the setpoint distance between aviation forbidden zone early warning line and aviation forbidden zone markings is according to the aviation
The real-time flight speed of device and set in real time, the setting between aviation forbidden zone early warning line and aviation forbidden zone markings away from
From the real-time flight speed v of >=airborne vehicleim/s×30s。
9. a kind of unattended aircraft information gathering transmission ground installation, it is characterised in that including airborne broadcast type
Automatic dependent surveillance device, radar, Automatic dependent surveillance broadcast device information collecting unit, radar information collecting unit, clothes
Business device and mobile terminal,
The airborne Automatic dependent surveillance broadcast device is loaded on the airborne vehicle, for obtaining the airborne vehicle in real time
Real-time flight information；
The real-time flight information that the radar passes through airborne vehicle described in radar wave real-time detection；
The Automatic dependent surveillance broadcast device information collecting unit is used to gather the automatic phase of aircraft onboard broadcast type in real time
The real-time flight information that monitoring arrangement is sent is closed, and the aircraft onboard Automatic dependent surveillance broadcast device got is sent
Real-time flight information real-time Transmission to the server；
The radar information collecting unit is used to gather the airborne vehicle real-time flight information arrived by radar wave detection in real time, and will
The real-time flight information real-time Transmission of the airborne vehicle arrived by radar wave detection got is to the server；
The server be used for by from the Automatic dependent surveillance broadcast device information collecting unit obtain by the broadcast
The real-time flight information that formula automatic dependent surveillance device is sent, and from radar information collecting unit acquisition by the thunder
Up to the airborne vehicle real-time detected by radar wave real-time flight information collect after send to the mobile terminal；
The mobile terminal is used to be believed according to the real-time flight sent by the Automatic dependent surveillance broadcast device got
Breath, and the real-time flight information of the airborne vehicle real-time detected from the radar by radar wave are sent out to the airborne vehicle
Send control instruction.
10. ground installation is transmitted according to the unattended aircraft information gathering of claim 9, it is characterised in that described
The electric supply installation of Automatic dependent surveillance broadcast device information collecting unit, radar information collecting unit and server includes photovoltaic
TRT, battery and power supply management chip,
When the Automatic dependent surveillance broadcast device information collecting unit described enough of electric energy caused by the photovoltaic power generation apparatus, thunder
Up to information acquisition unit and server in use, battery described in the power supply management chip controls is off；
When electric energy caused by the photovoltaic power generation apparatus is not enough to for Automatic dependent surveillance broadcast device information collection list
Member, radar information collecting unit and server in use, battery is in closure state described in the power supply management chip controls,
So that the difference electric energy of the Automatic dependent surveillance broadcast device information collecting unit, radar information collecting unit and server
Supplied by the batteries.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710817558.2A CN107564340A (en) | 2017-09-12 | 2017-09-12 | Unattended aircraft information gathering transmission surface process and device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
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