CN205353672U - Flight monitoring device , unmanned aerial vehicle and ground control station - Google Patents
Flight monitoring device , unmanned aerial vehicle and ground control station Download PDFInfo
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Abstract
The utility model mainly provides a flight monitoring device for for the unmanned aerial vehicle condition monitoring that flies, wherein, above -mentioned unmanned aerial vehicle is equipped with the detection device who is used for detecting its flight state parameter, and wherein, above -mentioned flight monitoring device includes: a data collection station for gathering above -mentioned detection device's detected signal, based on prestore reference conditions above that with the detected signal gathered and generate the watch -dog of above -mentioned unmanned aerial vehicle's running state information, with the network communication ports of above -mentioned running state information transmission to the third party service ware. Furthermore, the utility model discloses still provide unmanned aerial vehicle and ground control station including the aforesaid flight monitoring device. Adopt above -mentioned scheme, can make the unmanned aerial vehicle operator in time regularly maintain and carry out real -time fault monitoring above -mentioned unmanned aerial vehicle to improve unmanned aerial vehicle's flight factor of safety effectively, reduce the probability that unmanned aerial vehicle flight in -process broke down.
Description
Technical field
This utility model relates generally to unmanned air vehicle technique field, particularly relates to state of flight monitoring and the maintenance management aspect of unmanned plane.
Background technology
Owing to unmanned plane has the features such as volume is little, cost is low, range of activity is big, so that with the development of unmanned air vehicle technique, the use in people live of many rotary wind types unmanned plane is universal all the more, also allows for many people and enjoys flight manipulation experience.
But, no matter the integrated level of unmanned plane higher, modular member popularity rate is comprehensive again, it needs for being periodically subject to safeguard to improve its processing safety, reduces the probability that operator breaks down when flight manipulation.Especially flight assembly is easily caused loss by unmanned plane in flight course, if being irregularly maintained, then can be that the flight of unmanned plane brings great potential safety hazard.
But, major part flight operation person does not know about the problems such as some parts when needing that unmanned plane is safeguarded or understood unmanned plane are damaged, so often causing the existence that just can be appreciated that the problems referred to above during the situations such as unmanned plane falls in flight course, but, now day after the fair.
In order to solve the problems referred to above, Chinese patent CN201020232906.3 it is proposed that arrange health control device in the equipment manager of aircraft, wherein, this health control device includes failure diagnosis unit, failure predication unit, system reconfiguration unit and the fault detect and the isolated location that are connected with serial general-purpose interface spi bus；Failure diagnosis unit receives aircraft subsystem and the digital signal about respective running status of Integrated Electronic System transmission by spi bus, carries out fault diagnosis；Failure predication unit receives aircraft subsystem and the digital signal of Integrated Electronic System transmission by spi bus, carries out failure predication；System reconfiguration unit receives failure diagnosis unit and the fault type of failure predication unit transmission, carries out corresponding Breakdown Maintenance；Fault detect and isolated location receive the maintenance of system reconfiguration unit transmission and unsuccessfully indicate, to safeguarding that failed fault is isolated.So, adopt such scheme to be capable of aircraft and independently carry out health control.
But, the health control device structure of such scheme is numerous and diverse, it is necessary to building self maintenance or the platform safeguarded, manufacturing cost is higher, it is difficult to promote the use of on the unmanned plane that current popularity rate is higher.
For this, how can provide simply, at low cost for unmanned plane operator and in time unmanned plane be carried out periodic maintenance and/or unmanned plane exists operation exception and needs to carry out the prompting of the relevant informations such as maintenance and provide, for it, the relevant information carrying out the concrete ways such as maintenance and be easy on unmanned plane the demands such as popularization and application and be problem in the urgent need to address at present.
Utility model content
This utility model mainly provides a kind of and operator can be reminded in time unmanned plane to be safeguarded or detect and specifically safeguard that relevant information is to improve the flight supervising device of the safety coefficient of unmanned plane for its offer.In order to achieve the above object, this utility model mainly provides techniques below scheme:
A kind of flight supervising device, for carrying out state of flight monitoring for unmanned plane, wherein, described unmanned plane is provided with the detecting device for detecting its flight status parameter, and wherein, described flight supervising device includes:
Data acquisition unit, for gathering the detection signal of described detecting device；
Watch-dog, is connected with described data acquisition unit, and generates the running state information of described unmanned plane based on being stored in advance in base condition thereon and the detecting signal of described collection；
Network communications port, is connected with described watch-dog, and described running state information is transmitted to third-party server via described network communications port.
Further, described flight supervising device also includes one for receiving the order loader of external authorization order, and described order loader is connected with described watch-dog and described network communications port respectively.
Specifically, described third-party server is cloud server.
Specifically, described watch-dog includes being connected and store described base condition with described data acquisition unit memorizer and compare the comparator of relation between described detection signal and described base condition.
Specifically, described memorizer includes the first partition holding of the storage type I information relevant to described unmanned plane product attribute and stores and the second partition holding of Equations of The Second Kind information that described third-party server is correlated with.
Yet further, described flight supervising device is additionally provided with a display being connected to show described running state information with described watch-dog.
Further, described flight supervising device also includes a data sink being connected with described network communications port, and described data sink receives the feedback information corresponding with described running state information sent by described third-party server.
Further, described flight supervising device also includes an alarm being connected with described watch-dog.
In addition, this utility model also provides for a kind of unmanned plane, it is connected to detect the detecting device of its flight status parameter with described flight assembly including: the flight assembly performing flight operation, for the communication unit received and sent messages and be connected with described flight assembly to perform the control unit that flight controls according to the information received, wherein, described unmanned plane also includes arbitrary aforesaid flight supervising device, and described flight supervising device is all connected with described communication unit and described control unit.
Additionally, this utility model also provides for a kind of ground control station, unmanned plane is carried out flight control and monitoring, including: with the radio communication device that described unmanned plane interacts communication, it is connected with described radio communication device and generates the central processing unit of flight control instruction, wherein, described ground control station also includes arbitrary aforesaid flight supervising device, and described flight supervising device is connected with described radio communication device and described central processing unit respectively.
Adopt technique scheme, unmanned plane or ground control station can regularly remind operator in time unmanned plane to be carried out maintenance process, and remind operator to need unmanned plane is keeped in repair in time when Preliminary detection unmanned plane is abnormal, and simultaneously by carrying out above-mentioned maintenance process or keeping in repair the relevant information offers such as required concrete ways to operator so that operator can select concrete unmanned plane maintenance management service side, thus being greatly improved the safety coefficient of unmanned plane.
Accompanying drawing explanation
Fig. 1 is the composition schematic diagram of this utility model embodiment one unmanned plane；
Fig. 2 is the composition schematic diagram of this utility model embodiment one ground control station；
Fig. 3 is the composition schematic diagram of this utility model embodiment one flight supervising device；
Fig. 4 is the composition schematic diagram of this utility model embodiment one monitoring module；
Fig. 5 is that this utility model embodiment one is flown the schematic diagram of monitoring method；
Fig. 6 is a kind of particular flow sheet that this utility model embodiment one implements flight monitoring method；
Fig. 7 is the composition schematic diagram of this utility model embodiment two flight supervising device；
Fig. 8 is that this utility model embodiment two is flown the particular flow sheet of monitoring method.
Symbol description: 10 unmanned planes, 101 communication units, 102 control units, 103 flight assemblies, 104 detecting devices, 105 power supplys, 20 ground control stations, 201 power supply units, 202 radio communication devices, 203 flight supervising devices, 2031 data acquisition units, 2032 watch-dogs, 2032a memorizer, 2032b comparator, 2033 network communications port, 2034 output units, 2035 alarms, 2036 order loaders, 204 central processing units.
Detailed description of the invention
Main technical schemes of the present utility model is: by arranging flight supervising device, judge that unmanned plane is the need of carrying out General Maintenance or breakdown maintenance with the running state parameter of comparison unmanned plane and default base condition, notify the above-mentioned maintenance of operator or fault message in time, and above-mentioned information is sent to third-party server to allow the operator to obtain in time dependent help simultaneously；Thus can fully ensure that unmanned plane obtains periodic maintenance and on-call maintenance, it is greatly improved its security performance, reduces the probability broken down in unmanned plane during flying process, and, scheme is simple, with low cost, it is simple in the application of unmanned plane field.
Hereinafter only by the description of specific embodiment, the technical solution of the utility model made comprehensive, detailed description.It should be noted that these specific descriptions simply allow those of ordinary skill in the art be more prone to, clearly understand this utility model, but not to limited explanation of the present utility model.
Embodiment one:
Fig. 1 is the composition schematic diagram of the unmanned plane of the present embodiment.As it is shown in figure 1, unmanned plane 10 includes: the communication unit 101 of be used for receiving and sending messages (as received control instruction and sending corresponding feedback information etc.)；It is connected with above-mentioned communication unit 101 unmanned plane carries out the control unit 102 that flight controls according to received information；What perform above-mentioned control unit 102 controls the flight assembly 103 to perform flight operation, specifically, above-mentioned flight assembly 103 includes providing the motor of flying power for unmanned plane, receiving the power of above-mentioned motor and be converted to the fly propeller of required push-pull effort of unmanned plane 10 and be connected with motor and think that it provides the electron speed regulator etc. of low-voltage AC；The detecting device 104 detecting the flight status parameter of unmanned plane 10 in real time it is connected with above-mentioned flight assembly 103；Parts for constituting unmanned plane provide the power supply 105 of electric power.
Fig. 2 is the composition schematic diagram of the ground control station of the present embodiment.As shown in Figure 2, this ground control station 20 includes interconnective power supply unit 201, radio communication device 202 and central processing unit 204, so, it is possible to the UAV Flight Control instruction generated by central processing unit 204 transmits the communication unit 101 to above-mentioned unmanned plane 10 via radio communication device 202.
In order to remind in time unmanned plane operator regularly unmanned plane to be safeguarded and/or the fault of unmanned plane generation keep in repair to improve the safety coefficient of unmanned plane in time, preferably, as shown in Figure 2, in the present embodiment, being additionally provided with a flight supervising device 203 on above-mentioned ground control station 20, it is for carrying out monitor in real time to the state of flight of unmanned plane 10.As in figure 2 it is shown, above-mentioned flight supervising device 203 is all connected with above-mentioned radio communication device 202 and above-mentioned central processing unit 204.Specifically, as shown in Figure 3, above-mentioned flight supervising device 203 includes: gather the data acquisition unit 2031 of the detection signal of above-mentioned detection device 104, it is connected with above-mentioned data acquisition unit 2031 detect signal according to what gather and be stored in advance in base condition thereon and generate the watch-dog 2032 of the running state information of unmanned plane and be connected with above-mentioned watch-dog 2032 with the output unit 2034 above-mentioned running state information exported to outside, and preferably, above-mentioned output unit 2034 is for exporting outside for above-mentioned running state information to unmanned plane operator so that operator knows above-mentioned running state information in time.It will be recognized by one of ordinary skill in the art that above-mentioned flight supervising device can become one with central processing unit.Preferably, in order to allow the operator to learn in time the various relevant informations of unmanned plane 10, in the present embodiment, above-mentioned output unit 2034 can be the display device (not shown) such as display.
As shown in Figure 3, in order to while can provide the running state information of above-mentioned unmanned plane for operator, the relevant informations such as the concrete ways that carry out follow-up service based on above-mentioned status information also can be provided for operator, and supervise operator that unmanned plane carries out the operations such as maintenance management in time, preferably, in the present embodiment, above-mentioned flight supervising device 203 also includes being connected with above-mentioned watch-dog 2032 above-mentioned running state information is transmitted the network communications port 2033 to third-party server via communication network, wherein, this third-party server can be provided by unmanned plane manufacturer, or provided by the professional providing unmanned plane maintenance/maintenance service, or by providing the information service firm offer etc. of relevant advertisements information for unmanned plane, maintenance/maintenance the relevant information that can provide with unmanned plane is provided.Specifically, in the present embodiment, above-mentioned third-party server can be cloud server.So, unmanned plane operator both can understand the running status of unmanned plane in time, it is also possible to makes professional understand unmanned plane running status in time, and provides concrete proposals, in time unmanned plane is safeguarded.It is to say, information pushing mechanism can be set up between operator and maintainer by above-mentioned flight supervising device, it is possible to make relevant maintenance information interactive between the two parties with above-mentioned supervising device for intermediary, thus being greatly improved the security performance of unmanned plane.And, the simple in construction of flight supervising device, also allow for carrying out Technique Popularizing widely in unmanned plane field.
Fig. 4 is the composition schematic diagram of the monitoring module of the present embodiment.As shown in Figure 4, above-mentioned watch-dog 2032 includes: for prestoring the memorizer 2032a of said reference condition, and this memorizer 2032a is connected with above-mentioned data acquisition unit 2031, specifically, this memorizer 2032a can be nonvolatile memory, such as EEPROM (EEPROM), FRAM (ferroelectric memory) etc.；And for comparing whether the detection signal that between detection signal and the said reference condition received, relation receives with judgement meets pre-conditioned comparator 2032b, and this comparator 2032b is connected with above-mentioned output module 2034 or above-mentioned network communications port 2033.In addition, in order to enable above-mentioned unmanned plane running state information to be sent to corresponding guardian in time, preferably, in above-mentioned memorizer 2032a, also storage has the Equations of The Second Kind information relevant to above-mentioned third-party server, such as relevant informations such as the concrete title of third-party server, addresses of items of mail.Further, the related service information safeguarded to make operator know in time with held unmanned plane/keep in repair, preferably, above-mentioned memorizer 2032a also stores the relevant type I informations such as the man-machine product attribute of being and not being, such as contents such as the model of unmanned plane, time buying, accessory information, it is simple to third-party server provides corresponding, suitable information on services according to the particular community of unmanned plane.Correspondingly, above-mentioned memorizer 2032a is provided with the first partition holding storing above-mentioned type I information and stores the second partition holding of above-mentioned Equations of The Second Kind information.
Specifically, the detecting device 104 of above-mentioned unmanned plane can be the time set running the time for adding up above-mentioned unmanned plane, then now corresponding, said reference condition is preset the preset time value needed unmanned aerial vehicle periodic maintenance.Such as, said reference condition be set as when the unmanned plane during flying time reach N*10 little time (N >=1) time send the prompting message of " unmanned plane needs to be serviced " to operator, then when watch-dog 203 judges that the clocking value of above-mentioned time set reaches said reference condition, then promote above-mentioned output unit 2034 to export above-mentioned prompting message to operator, and utilize network communications port 2033 to send information such as the relevant models of above-mentioned information and unmanned plane to third-party server in the lump.It will be recognized by one of ordinary skill in the art that the time buying that above-mentioned time set and base condition can be configured as with above-mentioned unmanned plane is associated.
Or, above-mentioned detection device 104 is alternatively the sensing system of the operational factor for detecting above-mentioned unmanned plane during flying assembly 103, in the present embodiment, this sensing system indicates that the multiple sensors being arranged on unmanned plane, as being used for detecting the velocity sensor of the rotating speed of propeller, for detecting the voltage/current detection device of the voltage/current of motor output, for detecting the gyro sensor etc. of flight angle, and each sensor is all connected with control unit and corresponding aircraft member, and each sensor can work alone and detect the running state parameter of corresponding aircraft member in real time.Correspondingly, now said reference condition is the threshold range that the described sensing system prestored is properly functioning, and exactly, said reference condition is the threshold range that each sensor prestored detects when corresponding aircraft member is properly functioning.Such as, when performing throttle commands, unmanned plane should complete each propeller and rotate the function to drive unmanned plane to rise, and when performing underriding instruction, unmanned plane should realize the function of flight forward by adjusting the rotating speed of each propeller, so time base condition can be that unmanned plane normally perform the flight path of corresponding flight attitude sensor during above-mentioned two instruction interval, the threshold speed of velocity sensor is interval, and watch-dog 203 has only to the flight path that above-mentioned flight attitude sensor and velocity sensor detected and speed and above-mentioned pre-conditioned compares, if coincide, then judge above-mentioned unmanned plane normal operation；Otherwise, then above-mentioned unmanned plane operation exception is judged.So, above-mentioned watch-dog 203 is by comparing the real time detection signal being gathered each sensor and namely above-mentioned default threshold range can determine whether each aircraft member above-mentioned whether normal operation.
Or, when above-mentioned detection device 104 is the sensing system being arranged on above-mentioned unmanned plane, the signal feedback that said reference condition can be configured as with every flight control instruction and corresponding to the detecting device of this flight control instruction and action is associated, the feedback of the detection signal of aircraft member corresponding when receiving certain flight control instruction such as unmanned plane or feedback order etc..In like manner, said reference condition also may be set to unmanned plane and normally performs sensor feedback situation corresponding during above-mentioned two instruction or order, for instance, when judging that one of them velocity sensor does not have signal feedback namely to can determine whether that now above-mentioned propeller exists fault.And, by by base condition with detection signal order dependent, also have the effect that and monitor whether each functional realiey parts complete work according to default flow process according to from signal control source successively to the order of functional realiey parts (such as each aircraft member), can be accurately judged to produce the concrete parts that fault causes flow process to stop, thus report fault conditions accurately can also be provided to operator.
Fig. 5 is that the present embodiment utilizes above-mentioned flight supervising device to carry out the method flow diagram of flight monitoring.As it is shown in figure 5, above-mentioned flight monitoring method comprises the following steps:
S1: gather the flight status parameter of unmanned plane；
Specifically, this step mainly utilizes above-mentioned data acquisition unit 2031 to gather the flight status parameter of unmanned plane according to default interval, wherein, above-mentioned flight status parameter can include the signal feedback (if any feedback-less, associated order etc.) etc. of the operation time of unmanned plane 10, the operational factor (rotating speed etc. such as the voltage/current output valve of motor, propeller) of flight assembly 103, flight assembly 103.
S2: generate unmanned plane running state information according to the relation of above-mentioned flight status parameter and default base condition；
Specifically, this step mainly utilizes the comparator 2032b in watch-dog 2032 to compare to judge whether it meets default condition to generate above-mentioned running state information by above-mentioned data acquisition unit 2031 flight status parameter gathered and the base condition being stored in advance in memorizer 2032a.
S3: above-mentioned running state information is sent to third-party server via network communications port 2033.
Specifically, this step is main utilizes communication network to send above-mentioned status information to above-mentioned third-party server according to the Equations of The Second Kind information relevant to third-party server being stored in above-mentioned memorizer 2032a.
Fig. 6 is the flow chart of the concrete grammar being monitored for sensing system with the running status to unmanned plane for detecting device.As shown in Figure 6, first gather the real time detection signal of the sensing system of above-mentioned unmanned plane 10, namely the real time detection signal of each sensor is gathered, then, judge whether above-mentioned detection signal is arranged in above-mentioned default threshold range, if being positioned at, then it represents that the aircraft member corresponding with this detection signal is in normal operating condition；Otherwise, it means that this aircraft member is in abnormality, in time above-mentioned running state information is sent to operator and be simultaneously sent to third-party server.
Those of ordinary skill in the art it should be understood that, corresponding prompting message can be exported to operator in time for the ease of above-mentioned flight supervising device, above-mentioned sub module stored can store following information: the information relevant according to the running state parameter of flight control instruction and corresponding aircraft member one to one and the look-up table set up.
Additionally, in order to remind operator in time, it is preferable that above-mentioned flight supervising device 203 also includes an alarm 2035 being connected with above-mentioned watch-dog 2032, utilizes this alarm 2035 can be effectively improved operator's Vigilance to output result.This alarm 2035 can be sound alarm subsystem, light crossing-signal, audible-visual annunciator one or more, can select according to specific needs.
It will be recognized by one of ordinary skill in the art that above-mentioned detection device also can both include time set, also include sensor device.
It will be recognized by one of ordinary skill in the art that above-mentioned flight supervising device may also be arranged on unmanned plane, then now, above-mentioned flight supervising device is all connected with above-mentioned communication unit and control unit.Exactly, preferably, now above-mentioned output unit and above-mentioned communication unit become one, and the running state information that above-mentioned watch-dog generates can export to third-party server and ground control station via above-mentioned network communications port and above-mentioned communication unit respectively respectively.
Obviously, adopt above-mentioned flight supervising device, operator can be reminded in time to be periodically subject to unmanned plane in time safeguard and carry out malfunction monitoring, and the relevant information of the concrete ways that unmanned plane carries out maintenance management is provided for operator in time, thus being effectively improved the flight safety coefficient of unmanned plane, reduce the probability broken down in unmanned plane during flying process, and, it is simple to it is widely popularized in unmanned plane field.
Embodiment two:
The present embodiment and embodiment one are distinctive in that, as shown in Figure 7, in the present embodiment, above-mentioned flight supervising device 203 also includes an order loader 2036, this order loader 2036 is connected with above-mentioned watch-dog 2032, with the authorized order based on externally input by above-mentioned running state information transmission to network communications port 2033, namely above-mentioned running state information is transmitted to unmanned plane guardian via network communications port 2033 when obtaining the authorized order of unmanned plane operator input.Specifically; mentioned order loader 2036 is for receiving the authorized order of externally input; namely utilize the mentioned order loader 2036 can so that above-mentioned running state information can operate based on the confirmation of operator again outer send to third-party server (unmanned plane guardian); or send to its third-party server specified based on outside the confirmation again of operator; thus the privacy of operator can effectively be protected, it is to avoid leakage.
Fig. 8 is the flow chart of the flight monitoring method of the present embodiment.As shown in Figure 8, this flight monitoring method comprises the following steps:
S11: gather the flight status parameter of unmanned plane；Described by concrete operations such as previous embodiment one；
S12: generate the running state information of unmanned plane according to above-mentioned flight status parameter and default base condition；Described by concrete operations such as previous embodiment one；
S13: above-mentioned status information is sent to network communication module according to the authorized order of externally input；
S14: above-mentioned status information is sent to third-party server via above-mentioned network communications port 2033.
Such as, when above-mentioned prompting message (such as periodic maintenance, breakdown judge etc.) sends to operator, authorized order according to operator's input, namely, under allowing based on operator, above-mentioned status information is sent via network to default third-party server or the server specified so that follow-up carrying out special maintenance.
All the other contents are similar with embodiment one, and therefore not to repeat here.
Embodiment three:
The present embodiment differs primarily in that with embodiment one or two, in the present embodiment, above-mentioned flight supervising device is additionally provided with a data sink, and this data sink is connected with network communications port to receive the feedback information corresponding with above-mentioned running state information sent from third-party server.That is, third-party server can feed back corresponding information to flight supervising device according to the unmanned plane running state information received, so that unmanned plane operator not only can understand the running status of unmanned plane in time, professional's concrete proposals for unmanned plane running status can also be obtained in time, in time unmanned plane is safeguarded.
Preferably, in the present embodiment, above-mentioned data sink is also connected with above-mentioned output module (such as display devices such as display), in time the feedback information received is reflected into unmanned plane operator.
Corresponding, when utilizing above-mentioned flight supervising device that the state of flight of unmanned plane is monitored, further comprising the steps of: to receive from above-mentioned third-party server the feedback information corresponding with above-mentioned running state information.
And, specifically, above-mentioned data sink can be wireless receiver, Gbps serial receiver, infrared receiver etc., can select according to real needs.
All the other contents are similar with embodiment one or embodiment two, and therefore not to repeat here.
Each functional module in each embodiment of the application can be integrated in a processing unit, it is also possible to is that each functional module is individually physically present, it is also possible to two or more modules are inherited in a unit.Above-mentioned integrated unit both can adopt the form of hardware to realize, it would however also be possible to employ the form of SFU software functional unit realizes.
Last it should be noted that described above is only most preferred embodiment of the present utility model, not this utility model is done any pro forma restriction.Any those of ordinary skill in the art; without departing within the scope of technical solutions of the utility model; all may utilize the way of the disclosure above and technology contents and technical solutions of the utility model are made many possible variations and simple replacement etc., these broadly fall into the scope of technical solutions of the utility model protection.
Claims (10)
1. a flight supervising device, for carrying out state of flight monitoring for unmanned plane, wherein, described unmanned plane is provided with the detecting device for detecting its flight status parameter, it is characterised in that described flight supervising device includes:
Data acquisition unit, for gathering the detection signal of described detecting device；
Watch-dog, is connected with described data acquisition unit, and generates the running state information of described unmanned plane based on being stored in advance in base condition thereon and the detecting signal of described collection；
Network communications port, is connected with described watch-dog, and described running state information is transmitted to third-party server via described network communications port.
2. flight supervising device according to claim 1, it is characterised in that described flight supervising device also includes for receiving the order loader of external authorization order, and described order loader is connected with described watch-dog and described network communications port respectively.
3. flight supervising device according to claim 1 and 2, it is characterised in that memorizer that described watch-dog includes being connected and store described base condition with described data acquisition unit and compare the comparator of relation between described detection signal and described base condition.
4. flight supervising device according to claim 3, it is characterized in that, described memorizer includes the first partition holding of the storage type I information relevant to described unmanned plane product attribute and stores and the second partition holding of Equations of The Second Kind information that described third-party server is correlated with.
5. flight supervising device according to claim 4, it is characterised in that described flight supervising device is additionally provided with a display being connected to show described running state information with described watch-dog.
6. the flight supervising device according to claim 4 or 5, it is characterized in that, described flight supervising device also includes a data sink being connected with described network communications port, and described data sink receives the feedback information corresponding with described running state information sent by described third-party server.
7. the flight supervising device according to claim 4 or 5, it is characterised in that described flight supervising device also includes an alarm being connected with described watch-dog.
8. a unmanned plane, it is connected to detect the detecting device of its flight status parameter with described flight assembly including: the flight assembly performing flight operation, for the communication unit received and sent messages and be connected with described flight assembly to perform the control unit that flight controls according to the information received, it is characterized in that, described unmanned plane also includes the flight supervising device according to any claim in claim 1 to 7, and described flight supervising device is all connected with described communication unit and described control unit.
9. unmanned plane according to claim 8, it is characterised in that described detecting device is the sensing system of the operational factor detecting described flight assembly.
10. a ground control station, unmanned plane is carried out flight control and monitoring, including: with the radio communication device that described unmanned plane interacts communication, it is connected with described radio communication device and generates the central processing unit of flight control instruction, it is characterized in that, described ground control station also includes the flight supervising device according to any claim in claim 1 to 7, and described flight supervising device is connected with described radio communication device and described central processing unit respectively.
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| CN105607516A (en) * | 2016-01-07 | 2016-05-25 | 谭圆圆 | Flight monitoring device and flight state monitoring method |
| CN106343977A (en) * | 2016-09-21 | 2017-01-25 | 中国人民解放军国防科学技术大学 | UAV (unmanned aerial vehicle) operator state monitoring system based on multi-sensor fusion |
| CN106447184A (en) * | 2016-09-21 | 2017-02-22 | 中国人民解放军国防科学技术大学 | Unmanned aerial vehicle operator state evaluation method based on multi-sensor measurement and neural network learning |
| CN106447184B (en) * | 2016-09-21 | 2019-04-05 | 中国人民解放军国防科学技术大学 | Unmanned plane operator's state evaluating method based on multisensor measurement and neural network learning |
| CN106343977B (en) * | 2016-09-21 | 2019-07-09 | 中国人民解放军国防科学技术大学 | Unmanned plane operator's condition monitoring system based on Multi-sensor Fusion |
| CN106516159A (en) * | 2016-12-09 | 2017-03-22 | 中电科航空电子有限公司 | Airborne Aircraft Communication Addressing and Reporting System (ACARS) and malfunction diagnosis and health management method thereof |
| CN106970642A (en) * | 2017-04-20 | 2017-07-21 | 佛山科学技术学院 | A kind of multi-rotor unmanned aerial vehicle state monitoring apparatus |
| CN107132313A (en) * | 2017-05-08 | 2017-09-05 | 南京信息工程大学 | The method and pollution sources Check System of a kind of unmanned plane investigation pollution sources |
| CN108082478A (en) * | 2017-12-16 | 2018-05-29 | 佛山市神风航空科技有限公司 | A kind of early warning type unmanned plane monitors Reconnaissance system |
| CN108681334A (en) * | 2018-05-10 | 2018-10-19 | 上海乾达农业科技有限公司 | A kind of device for the unmanned machine operation supervision of agricultural plant protection |
| CN111831487A (en) * | 2019-04-15 | 2020-10-27 | 丰鸟航空科技有限公司 | Data source output method, device, system and storage medium |
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