CN115421510A - Cruise unmanned aerial vehicle system with high cruise capacity - Google Patents
Cruise unmanned aerial vehicle system with high cruise capacity Download PDFInfo
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- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
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Abstract
The invention relates to the technical field of unmanned aerial vehicles, and particularly discloses a cruise unmanned aerial vehicle system with high cruise capacity, which comprises: host system, the module is solved to the flight route, switching interface module, weighing module, battery energy module and cruising ability calculation module, add the total weight that obtains unmanned aerial vehicle through the weight of battery that cruising ability calculation module obtained unmanned aerial vehicle's dead weight and weighing module, flight distance according to unmanned aerial vehicle, high, speed, the electric quantity that unmanned aerial vehicle flight needs is predicated to wind speed and unmanned aerial vehicle total weight, compare the electric quantity that unmanned aerial vehicle needs and the energy of the battery that obtains from battery energy module, when the electric quantity that unmanned aerial vehicle needs is less than or equal to the threshold value of the energy of battery, recommend to use the battery to cruise, otherwise, it cruises not to recommend the battery. Therefore, the invention improves the inspection capability of the unmanned aerial vehicle by selecting a more suitable battery for inspection, and solves the problem of insufficient inspection capability of the unmanned aerial vehicle used in the conventional power inspection.
Description
Technical Field
The invention belongs to the technical field of unmanned aerial vehicles, and particularly relates to a cruise unmanned aerial vehicle system with high cruise capacity.
Background
The unmanned aerial vehicle is mostly applied to pursuing large load, and high reliability is realized in long voyage, so that the main requirement on the unmanned aerial vehicle battery is that the energy density is high and the power density is high. The lithium battery has excellent discharge characteristics, which makes the lithium battery the most important power storage unit in the field of electric unmanned aerial vehicles. At present, in the field of commercial unmanned aerial vehicles, lithium polymer batteries become the most ideal secondary battery of the unmanned aerial vehicle with high cost performance. With the rapid development of the application market of the unmanned aerial vehicle, the requirements on various indexes of an unmanned aerial vehicle power system are higher and higher, particularly the indexes during navigation. In the whole flight envelope, the electric unmanned aerial vehicle may have large power requirements at each stage, especially at the end of a mission. And along with the progress of lithium cell discharge process, the lithium cell discharge capacity tends to weaken, and this is very unfavorable to unmanned aerial vehicle flight task. Therefore, when the battery with the appropriate capacity is configured for the electric unmanned aerial vehicle, careful consideration needs to be given to the battery, and the requirements of each flight phase on the power are within the output capacity range of the lithium battery.
Unmanned aerial vehicle on the existing market uses many rotor unmanned aerial vehicle as the owner, and mainly choose for use the electric energy as the main energy, the lithium cell becomes one of the important choices of electronic unmanned aerial vehicle power source, many rotor unmanned aerial vehicle theory of operation is simple, can the VTOL, do not need the runway, it is little to the requirement in place, hover in the air easily moreover, many rotor unmanned aerial vehicle's main movable part is exactly the motor simultaneously, the reliability is than higher, and simple structure is convenient for renewal part. These advantages are the reasons that many rotor unmanned aerial vehicles stand out in civilian unmanned aerial vehicle field. And when many rotor unmanned aerial vehicle's function is more and more powerful, its duration just needs to attach more attention. Unmanned aerial vehicle is along with the change of flight condition at the flight in-process, also changes along with it to the energy output demand of lithium cell, and the continuation of the journey of many rotor unmanned aerial vehicle of selling on the existing market is at twenty several minutes basically, and some unmanned aerial vehicle have only ten several minutes's duration even, and this is not enough far away for being used for electric power to patrol and examine the function that uses many rotor unmanned aerial vehicle. Therefore, a cruise drone system with high cruise capability is needed, which can perform self-detection to obtain higher cruise capability.
Disclosure of Invention
The invention aims to provide a cruising unmanned aerial vehicle system with high cruising ability, so as to overcome the defect of insufficient cruising ability of an unmanned aerial vehicle used for the conventional power patrol.
In order to achieve the above object, the present invention provides a cruise drone system with high cruise capability, including:
the main control module is used for controlling the unmanned aerial vehicle to take off according to the received signal and storing basic data of the unmanned aerial vehicle;
the flight path calculation module is used for acquiring a preset flight path of the unmanned aerial vehicle and calculating the flight distance, the flight height and the flight speed of the unmanned aerial vehicle;
the adapter interface module is used for connecting various types of batteries and transmitting current to the main control module;
the weighing module is arranged on the unmanned aerial vehicle and used for weighing the battery to obtain the weight of the battery;
the battery energy module is used for acquiring the energy of the battery; and
cruise ability calculation module for add the total weight that obtains unmanned aerial vehicle with unmanned aerial vehicle's dead weight and the weight of the battery that weighing module acquireed, acquire the wind speed through the weather forecast, and predict the required electric quantity of unmanned aerial vehicle flight according to unmanned aerial vehicle's flying distance, altitude, flying speed, wind speed and unmanned aerial vehicle total weight, will the electric quantity that unmanned aerial vehicle needs compares with the energy of the battery that acquires from battery energy module, when the electric quantity that unmanned aerial vehicle needs is less than or equal to the threshold value of the energy of battery, recommends the use the battery cruises, otherwise, does not recommend the battery cruises.
Further, the basic data of the unmanned aerial vehicle comprises: the flight path, self weight, flight speed, flight state and ambient temperature of unmanned aerial vehicle.
Further, the method for predicting the electric quantity required by the unmanned aerial vehicle comprises the following steps:
enabling the unmanned aerial vehicle to respectively carry out basic distance flight under the flight conditions of different temperatures, different flight heights, different flight speeds, different wind speeds and different total weight of the unmanned aerial vehicle, and recording the electric quantity consumed by the unmanned aerial vehicle during flight;
repeating the previous step, enabling the unmanned aerial vehicle to fly on a plurality of times of flight paths with different basic distances, recording the electric quantity consumed by the unmanned aerial vehicle, judging whether the different flight distances are equal to the multiple of the energy consumed by the flight of the basic distances, respectively recording the energy consumed by the flight of the basic distances when the different flight distances are equal to the multiple of the energy consumed by the flight of the basic distances, and otherwise, storing all data of the energy consumed by the unmanned aerial vehicle under different flight conditions based on the actual measurement;
constructing an adaptive neural fuzzy inference model, wherein the output of the adaptive neural fuzzy inference model is the electric quantity consumed by the unmanned aerial vehicle
Inputting the stored historical number into the adaptive neural fuzzy inference model, and training and verifying the adaptive neural fuzzy inference model to obtain an electric quantity prediction model capable of predicting the electric quantity consumed by the unmanned aerial vehicle;
and preprocessing the real-time data of the unmanned aerial vehicle acquired in real time, and predicting through an electric quantity prediction model so as to obtain the electric quantity required by the unmanned aerial vehicle in flight.
Further, the fuzzy set types adopted by the input quantity of the adaptive neural fuzzy inference model comprise: temperature, wind speed, flight speed, total weight, and flight distance; real-time data of the unmanned aerial vehicle include: flight distance, flight altitude, flight speed, wind speed, and unmanned aerial vehicle total weight.
Furthermore, the cruise capacity calculation module respectively calculates the cruise capacity of each type of battery, the value of the energy required by the unmanned aerial vehicle in the energy of the battery is used as the cruise capacity value obtained by combining the unmanned aerial vehicle with the battery, and the cruise capacity sequence of each type of battery relative to the unmanned aerial vehicle is obtained through the cruise capacity value sequence.
Further, the drone includes: the unmanned aerial vehicle comprises a machine arm, a mounting box, a foot support and a camera, wherein the mounting box is used for storing a circuit module of the unmanned aerial vehicle; the plurality of machine arms are symmetrically arranged on the periphery of the mounting box; the foot bracket is arranged below the mounting box; the camera is installed at one side of the installation box.
Further, a battery box is arranged below the mounting box and comprises a box body and a cover body, and the box body is of a hollow structure with an opening on the side surface; the cover body is rotatably connected with the box body, a bulge is arranged on one side of the cover body facing the opening of the box body, the bulge is matched with the opening of the cover body and the box body, and a circle of rubber is arranged on the outer side of the bulge; and a battery mounting bracket is arranged in the battery box, and various types of batteries are placed through the battery mounting bracket.
Further, the battery mounting bracket is slidably mounted in the battery box.
Compared with the prior art, the invention has the following beneficial effects:
the invention provides a cruise unmanned aerial vehicle system with high cruise capacity, which comprises: the main control module is used for controlling the unmanned aerial vehicle to take off according to the received signal and storing basic data of the unmanned aerial vehicle; the flight path resolving module is used for acquiring a flight path of a preset unmanned aerial vehicle and calculating the flight distance, the flight height and the flight speed of the unmanned aerial vehicle; the adapter interface module is used for being connected with various types of batteries and transmitting current to the main control module; the weighing module is arranged on the unmanned aerial vehicle and used for weighing the battery to obtain the weight of the battery; the battery energy module is used for acquiring the energy of the battery; the weight of the battery that obtains unmanned aerial vehicle through cruising ability calculation module dead weight and weighing module of unmanned aerial vehicle adds obtains unmanned aerial vehicle's total weight, acquires the wind speed through the weather forecast to according to unmanned aerial vehicle's flying distance, altitude, flying speed, the electric quantity that the flight of unmanned aerial vehicle needs is predicted to unmanned aerial vehicle total weight, will the electric quantity that unmanned aerial vehicle needs compares with the energy of the battery that obtains from battery energy module, and when the electric quantity that unmanned aerial vehicle needs was less than or equal to the threshold value of the energy of battery, the recommendation was used the battery cruises, otherwise, does not recommend the battery cruises. Therefore, the invention improves the inspection capability of the unmanned aerial vehicle by selecting a more suitable battery for inspection, and solves the problem of insufficient inspection capability of the unmanned aerial vehicle used in the conventional power inspection.
2. According to the unmanned aerial vehicle, the battery box is arranged below the mounting box, the battery mounting bracket is mounted in the battery box, and various types of batteries are placed through the battery mounting bracket, so that the unmanned aerial vehicle is more convenient than the battery is directly replaced in the structure of the unmanned aerial vehicle body.
Drawings
In order to more clearly illustrate the technical solution of the present invention, the drawings needed to be used in the description of the embodiments are briefly introduced below, and it is obvious that the drawings in the following description are only one embodiment of the present invention, and it is obvious for those skilled in the art to obtain other drawings based on the drawings without creative efforts.
Fig. 1 is a schematic mechanical diagram of a drone of one embodiment of the present invention;
FIG. 2 is a schematic structural diagram of the high cruise capability cruise drone system of the present invention;
FIG. 3 is a schematic structural view of a battery mounting bracket of the present invention;
FIG. 4 is a schematic view of the stop of the present invention;
wherein: 1. mounting a box; 2. a camera; 3. a horn; 4. a foot support; 5. a battery case;
6. a battery mounting bracket; 61. a frame body; 62. a base plate; 63. heat dissipation holes; 64. a groove; 65. a first support bar; 66. a second support bar; 68. positioning holes; 69. a slider;
67. a stopper; 671. an upper portion; 672. a lower part.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
In the description of the present invention, it should be noted that the terms "central", "longitudinal", "lateral", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "top", "bottom", "inner", "outer", etc. indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplicity of description, but do not indicate or imply that the device or element referred to must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention.
In the description of the present invention, the meaning of a plurality of means is one or more, the meaning of a plurality of means is two or more, and larger, smaller, larger, etc. are understood as excluding the number, and larger, smaller, inner, etc. are understood as including the number. The terms "first", "second" and "third", if any, are used for descriptive purposes only and for distinguishing between technical features and are not to be construed as indicating or implying relative importance or implying a number of indicated technical features or a precedence of indicated technical features.
In the description of the present invention, it should be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "disposed" are to be construed broadly and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art. The following describes an embodiment of the present invention based on its overall structure.
As shown in fig. 1, a high ability of cruising unmanned aerial vehicle system includes the unmanned aerial vehicle body, and unmanned aerial vehicle's body includes: the device comprises a machine arm 3, a mounting box 1, a foot support 4 and a camera 2; the plurality of machine arms 3 are symmetrically arranged around the mounting box 1, wherein four machine arms 3 can be adopted; foot support 4 installs in the below of mounting box 1, and foot support 4 can be selected as required, for example, adopts two I-shaped foot supports 4, and the below at mounting box 1 is installed to 4 symmetries of then two foot supports, and camera 2 then installs in one side of mounting box 1, can be located two adjacent horn 3 in the centre, and be located the place ahead when unmanned aerial vehicle flies, shoots when conveniently patrolling and examining. The mounting box 1 is used for storing basic circuits of unmanned aerial vehicles such as a main control module of the unmanned aerial vehicle, a battery, a high-precision positioning information receiver and wireless communication, and different batteries can be installed on the mounting box 1. Unmanned aerial vehicle in this application adopts many rotor unmanned aerial vehicle.
In order to provide unmanned aerial vehicle's cruising ability, the battery can adopt the glass compound that lithium, sodium were made to be the conducting substance, replaces the electrolyte of lithium cell in the past, can promote the energy density of lithium cell greatly, and the promotion of energy density has obvious effect to the continuation of the journey mileage equally.
In order to manage the battery of unmanned aerial vehicle, consequently, high cruise ability's unmanned aerial vehicle system that cruises still includes battery management module, and battery management module is used for carrying out the management suggestion of regularly charging and discharging to the battery, effectively manages battery life cycle number and life.
Wherein, host system is used for taking off according to the signal control unmanned aerial vehicle of receiving, stores unmanned aerial vehicle's basic data and real-time data, and wherein, unmanned aerial vehicle's basic data includes unmanned aerial vehicle's flight route, self weight, flight status and ambient temperature, and real-time data includes unmanned aerial vehicle's flying speed, the image that camera 2 shot etc..
In addition, the cruise unmanned aerial vehicle system can also select the most appropriate battery for the self-adaptive judgment of the connected batteries so that the unmanned aerial vehicle achieves the highest optimal cruise capacity, and therefore, the cruise unmanned aerial vehicle system further comprises:
the flight path calculation module is used for acquiring a preset flight path of the unmanned aerial vehicle and calculating the flight distance and the height of the unmanned aerial vehicle;
the adapter interface module can be connected with various types of batteries and transmits current to the main control module, and in order to prevent the current of the connected battery from being overlarge, the adapter interface module can be connected with a filtering or current limiting module and the like for current limitation after being switched;
the weighing module is arranged at the bottom of the mounting box 1 for placing the battery and is used for weighing the battery to obtain the weight of the battery; because the weighing module belongs to the consumable module, in order to prolong the service life of the weighing module, a telescopic result can be arranged at the bottom of the mounting box 1, so that the weighing module can not be in contact with a power supply when not in use;
the battery capacity detector is externally arranged when the adopted battery capacity detector is too large, and data is input through a handheld terminal of the unmanned aerial vehicle and then is sent to the unmanned aerial vehicle main control module after measurement;
cruise ability calculation module, cruise ability calculation module adds the weight that obtains unmanned aerial vehicle with unmanned aerial vehicle's dead weight and battery, acquire the wind speed through the weather forecast, and according to unmanned aerial vehicle's flying distance, flight height, flying speed, the electric quantity that unmanned aerial vehicle flight needs is come to prediction to wind speed and unmanned aerial vehicle total weight, compare the electric quantity that unmanned aerial vehicle needs with the energy of the battery that obtains from battery energy module, when the electric quantity that unmanned aerial vehicle needs is less than or equal to the threshold value of the energy of battery, recommend to use the battery cruises, otherwise, do not recommend the battery cruises.
Specifically, when the electric quantity that unmanned aerial vehicle needs is less than or equal to 80% of the energy of battery, unmanned aerial vehicle can use this battery to cruise, do not consider here to say that must 100% or 90%, because data are the prediction and get, need reserve some electric quantities for unmanned aerial vehicle to the energy consumption that causes such as accident or weather environment change is too big, and concrete setting also can set up littleer or bigger as required, only regards as the optimal data selection here.
The method for predicting the electric quantity required by the flight of the unmanned aerial vehicle comprises the following steps:
a11, enabling the unmanned aerial vehicle to respectively carry out basic distance flight under the flight conditions of different temperatures, different flight heights, different flight speeds, different wind speeds and different total weight of the unmanned aerial vehicle, and recording the electric quantity consumed by the unmanned aerial vehicle during flight;
a12, repeating the previous step, enabling the unmanned aerial vehicle to fly on a plurality of flight paths with different basic distances, recording the electric quantity consumed by the unmanned aerial vehicle, further confirming whether different flight distances of the unmanned aerial vehicle can be equal to the energy multiple consumed by the flight of the basic distances under the same flight condition, if so, respectively recording the energy consumed by the flight of the basic distances, otherwise, storing all data of the energy consumed by the unmanned aerial vehicle under different flight conditions based on the actual measurement;
a13, constructing an adaptive neuro-fuzzy inference model, wherein the fuzzy set type adopted by the input quantity of the adaptive neuro-fuzzy inference model comprises the following steps: temperature, wind speed, flying speed, total weight and flying distance are respectively A i 、B i 、C i 、D i 、E i (ii) a The output of the adaptive neural fuzzy inference model is the electric quantity consumed by the unmanned aerial vehicle, therefore, the data set is 5 fuzzy sets according to the input, the corresponding maximum number is 5 rules, and the fuzzy relation of the ith cabinet is as follows:
R i ＝A i ×B i ×C i ×D i ×E i ，f Ri ＝min{f Ai 、f Bi 、f Ci 、f Di 、f Ei }；
a14, arranging data stored in the data according to the input quantity of the adaptive neural fuzzy inference model, and training and verifying the adaptive neural fuzzy inference model to obtain an electric quantity prediction model capable of predicting the electric quantity consumed by the unmanned aerial vehicle;
a15, the flight distance, the flight height, the flight speed, the wind speed and the total weight of the unmanned aerial vehicle which are acquired in real time are preprocessed, and the prediction is carried out through an electric quantity prediction model, so that the electric quantity required by the flight of the unmanned aerial vehicle can be obtained.
In addition, the cruising ability calculation module carries out cruising ability calculation to each type of battery respectively, the value of the energy that occupies the battery according to unmanned aerial vehicle needs is as the cruising ability value that unmanned aerial vehicle combines this battery to obtain, cruising ability value sequences, cruising ability value is the best more between 50-80%, specific selection can set up as required, it should not regard as best or can use the ranking to be less than 50% cruising ability value, when being less than 50% then explain probably big or small using, the unmanned aerial vehicle that does not need so strong cruising ability carries out the task in reality. The invention provides a method for controlling the endurance of an unmanned aerial vehicle, which comprises the following steps: the method for estimating the cruising ability of the unmanned aerial vehicle comprises the steps of estimating the cruising ability of the unmanned aerial vehicle by the self weight, the flying speed, the flying state, the ambient temperature, the battery parameters and the like of the unmanned aerial vehicle, and accordingly selecting the most appropriate power supply to improve the circulation ability of the unmanned aerial vehicle.
As shown in fig. 2, although the mounting box 1 can mount different batteries, in order to facilitate mounting of various types of batteries, a battery box 5 is disposed below the mounting box 1, the battery box 5 includes a box body and a cover body, and the box body is a hollow structure with an opening on the side; the cover body is rotatably connected with the box body, one side of the cover body, facing the opening of the box body, is provided with a bulge, the bulge is matched with the opening of the cover body and the box body, and in order to ensure the sealing property, a circle of rubber is arranged on the outer side of the bulge, so that the waterproof effect can be realized through the rubber;
as shown in fig. 3, a battery mounting bracket 6 is mounted in the battery case 5, and the battery mounting bracket 6 includes: the battery box comprises a frame body 61, wherein the frame body 61 is a rectangular parallelepiped frame, the bottom of the frame body 61 is a bottom plate 62, a heat dissipation hole 63 is formed in the bottom, and the bottom plate 62 is used for accommodating a battery;
a stopper 67, the stopper 67 can be installed in the heat dissipation hole 63, the battery can be placed near the battery to move, as shown in fig. 4, the stopper 67 is an upper part and a lower part, the upper part 671 is fixedly connected with the lower part, wherein, the lower part is matched with the heat dissipation hole 63 and can be cylindrical; the upper part 671 is selected according to the side structure of the battery, and can be a cuboid or a cylinder, or a circular arc or a right-angle shape, and the like, and only one structure is illustrated in the figure; batteries with different shapes can be conveniently placed through the combination of the stop block 67 and the heat dissipation hole 63;
the weighing device comprises a groove 64, a groove 64 is formed in the middle of the bottom plate 62, a telescopic support is arranged in the middle of the bottom of the groove 64 and is an electric control telescopic support, a weighing module is installed at the top of the telescopic support and can be selected as required, the weighing module comprises a weighing sensor, a wireless transmission module and a weighing power supply, the weighing sensor and the wireless transmission module are respectively connected with the weighing power supply, the weighing sensor is connected with the wireless transmission module, and the telescopic support can ascend according to the control of the wireless transmission module to enable the weighing sensor to be higher than the top surface of the bottom plate 62; a push switch may also be provided at the top, which is depressed when the battery is on the bottom plate 62, and the telescoping bracket is powered on, so that the load cell extends out of the recess 64 above the top surface of the bottom plate 62;
at least one first supporting rod 65 is arranged on the left side and the right side of the frame body 61, and the first supporting rods 65 on the two sides are parallel to each other and parallel to one side edge of the frame body 61;
at least one second support bar 66 is arranged on the front side and the rear side of the frame body 61, and the second support bars 66 on the two sides are parallel to each other and parallel to one side edge of the frame body 61;
a plurality of mounting holes are formed in the tops of the first supporting rod 65 and the second supporting rod 66 and are uniformly arranged along the central axis of the supporting rods;
the two first support rods 65 and the two second support rods 66 can form a square frame parallel to the bottom plate 62, so that the frame is more stable; a plurality of second support rods 66 can be installed on two first support rods 65 on the same horizontal plane, a support plate can be formed on the two first support rods 65 and the plurality of second support rods 66 installed on the first support rods 65, and used for placing batteries or other modules, etc., the same principle as that of the first support rods 65 is set on the two second support rods on the same horizontal plane, when articles are placed on the first support rods 65 and the second support rods 66, the first support rods 65 and the second support rods 65 can be superposed on the first support rods 65 and/or the second support rods for fixing, or the fixing is performed through other stoppers 67, etc.;
the sliding blocks 69 are respectively installed on the outer sides of the left side and the right side of the frame body 61, corresponding sliding rails are correspondingly arranged on the inner sides of the battery boxes 5, and the battery installing supports 6 can be more easily placed in the battery boxes 5 and can be used for fixing the battery installing supports 6 by sliding the sliding blocks 69 on the sliding rails; in addition, in order to stably place the battery mounting bracket 6 in the battery box 5, a slider 69 may be provided on the outer side of the first support rod 65.
More types of batteries can be placed through the battery mounting bracket 6 to enable the unmanned aerial vehicle to achieve higher cruising ability.
The foregoing description of the specific exemplary embodiments of the invention has been presented for the purposes of illustration and description and is not intended to limit the invention to the precise form disclosed, and obviously many modifications and variations are possible in light of the above teaching, although examples of the invention have been shown and described, the present examples are intended to be illustrative only and not limiting of the invention, the particular features, structures, materials or characteristics described may be suitably combined in any one or more of the examples or illustrations, the exemplary embodiments were chosen and described in order to explain certain principles of the invention and its practical application, to thereby enable others skilled in the art to make modifications, substitutions, variations and alterations as are suited to the particular use contemplated without departing from the principles and spirit of the invention, and are intended to be protected by the following claims.
Claims (8)
1. A high cruise capability cruise unmanned aerial vehicle system, comprising:
the main control module is used for controlling the unmanned aerial vehicle to take off according to the received signal and storing basic data of the unmanned aerial vehicle;
the flight path calculation module is used for acquiring a preset flight path of the unmanned aerial vehicle and calculating the flight distance, the flight height and the flight speed of the unmanned aerial vehicle;
the adapter interface module is used for connecting various types of batteries and transmitting current to the main control module;
the weighing module is arranged on the unmanned aerial vehicle and used for weighing the battery to obtain the weight of the battery;
the battery energy module is used for acquiring the energy of the battery; and
cruise ability calculation module for add the total weight that obtains unmanned aerial vehicle with unmanned aerial vehicle's dead weight and the weight of the battery that weighing module acquireed, acquire the wind speed through the weather forecast, and predict the required electric quantity of unmanned aerial vehicle flight according to unmanned aerial vehicle's flying distance, altitude, flying speed, wind speed and unmanned aerial vehicle total weight, will the electric quantity that unmanned aerial vehicle needs compares with the energy of the battery that acquires from battery energy module, when the electric quantity that unmanned aerial vehicle needs is less than or equal to the threshold value of the energy of battery, recommends the use the battery cruises, otherwise, does not recommend the battery cruises.
2. The high cruise capacity cruise drone system according to claim 1, characterised in that said basic drone data comprises: the flight path, self weight, flight speed, flight state and ambient temperature of unmanned aerial vehicle.
3. A high cruise capability cruise drone system according to claim 1, characterised in that predicting the amount of electricity needed for the drone to fly comprises the following steps:
enabling the unmanned aerial vehicle to respectively carry out basic distance flight under the flight conditions of different temperatures, different flight heights, different flight speeds, different wind speeds and different total weight of the unmanned aerial vehicle, and recording the electric quantity consumed by the unmanned aerial vehicle during flight;
repeating the previous step, enabling the unmanned aerial vehicle to fly on a plurality of times of flight paths with different basic distances, recording the electric quantity consumed by the unmanned aerial vehicle, judging whether the different flight distances are equal to the multiple of the energy consumed by the flight of the basic distances, respectively recording the energy consumed by the flight of the basic distances when the different flight distances are equal to the multiple of the energy consumed by the flight of the basic distances, and otherwise, storing all data of the energy consumed by the unmanned aerial vehicle under different flight conditions based on the actual measurement;
constructing an adaptive neural fuzzy inference model, wherein the output of the adaptive neural fuzzy inference model is the electric quantity consumed by the unmanned aerial vehicle
Inputting the stored historical number into the adaptive neural fuzzy inference model, and training and verifying the adaptive neural fuzzy inference model to obtain an electric quantity prediction model capable of predicting the electric quantity consumed by the unmanned aerial vehicle;
and preprocessing the real-time data of the unmanned aerial vehicle acquired in real time, and predicting through an electric quantity prediction model so as to obtain the electric quantity required by the unmanned aerial vehicle in flight.
4. The high cruise capacity cruise drone system according to claim 3, characterised in that the fuzzy set type adopted by the input quantities of the adaptive neuro-fuzzy inference model comprises: temperature, wind speed, flight speed, total weight, and flight distance; real-time data of the unmanned aerial vehicle include: flight distance, flight altitude, flight speed, wind speed, and unmanned aerial vehicle total weight.
5. The cruise unmanned aerial vehicle system with high cruise capacity as claimed in claim 1, wherein the cruise capacity calculation module performs cruise capacity calculation on each type of battery respectively, and obtains the cruise capacity sequence of each type of battery relative to the unmanned aerial vehicle through cruise capacity value sequencing according to a cruise capacity value obtained by combining the battery with the unmanned aerial vehicle as a value of energy required by the unmanned aerial vehicle occupying the energy of the battery.
6. A high cruise capability cruise drone system according to claim 1, characterised in that said drone comprises: the unmanned aerial vehicle comprises a machine arm, a mounting box, a foot support and a camera, wherein the mounting box is used for storing a circuit module of the unmanned aerial vehicle; the plurality of machine arms are symmetrically arranged on the periphery of the mounting box; the foot bracket is arranged below the mounting box; the camera is installed at one side of the installation box.
7. The high-cruise-capability cruise unmanned aerial vehicle system according to claim 6, wherein a battery box is arranged below the mounting box, the battery box comprises a box body and a cover body, and the box body is of a hollow structure with an opening on the side surface; the cover body is rotatably connected with the box body, a bulge is arranged on one side of the cover body facing the opening of the box body, the bulge is matched with the opening of the cover body and the box body, and a circle of rubber is arranged on the outer side of the bulge; and a battery mounting bracket is arranged in the battery box, and various types of batteries are placed through the battery mounting bracket.
8. The high cruise capacity cruise drone system according to claim 7, wherein said battery mounting bracket is slidably mounted within said battery box.
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| Application Number | Priority Date | Filing Date | Title |
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| CN202210941236.XA CN115421510A (en) | 2022-08-05 | 2022-08-05 | Cruise unmanned aerial vehicle system with high cruise capacity |
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| CN202210941236.XA CN115421510A (en) | 2022-08-05 | 2022-08-05 | Cruise unmanned aerial vehicle system with high cruise capacity |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116625379A (en) * | 2023-07-25 | 2023-08-22 | 深圳深海创新技术有限公司 | Unmanned aerial vehicle, return electric quantity adjusting method and device thereof and flight controller |
| CN117217739A (en) * | 2023-11-07 | 2023-12-12 | 厦门闽投科技服务有限公司 | Intelligent electric power inspection system |
-
2022
- 2022-08-05 CN CN202210941236.XA patent/CN115421510A/en not_active Withdrawn
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116625379A (en) * | 2023-07-25 | 2023-08-22 | 深圳深海创新技术有限公司 | Unmanned aerial vehicle, return electric quantity adjusting method and device thereof and flight controller |
| CN116625379B (en) * | 2023-07-25 | 2023-10-24 | 深圳深海创新技术有限公司 | Unmanned aerial vehicle, return electric quantity adjusting method and device thereof and flight controller |
| CN117217739A (en) * | 2023-11-07 | 2023-12-12 | 厦门闽投科技服务有限公司 | Intelligent electric power inspection system |
| CN117217739B (en) * | 2023-11-07 | 2024-02-23 | 厦门闽投科技服务有限公司 | Intelligent electric power inspection system |
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Application publication date: 20221202 |