CN220933393U - Unmanned aerial vehicle based on autonomous obstacle avoidance flight of route planning - Google Patents
Unmanned aerial vehicle based on autonomous obstacle avoidance flight of route planning Download PDFInfo
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- CN220933393U CN220933393U CN202323089228.6U CN202323089228U CN220933393U CN 220933393 U CN220933393 U CN 220933393U CN 202323089228 U CN202323089228 U CN 202323089228U CN 220933393 U CN220933393 U CN 220933393U
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Abstract
The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle capable of independently avoiding obstacle flight based on route planning, which comprises a body, a rotating motor, a propeller, a control center, a telescopic motor, a foot rest, a storage battery pack, a telescopic antenna and an independent avoidance assembly.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle based on route planning autonomous obstacle avoidance flight.
Background
Unmanned aerial vehicles are hot in the prior art, and are popular with consumers due to the fact that the unmanned aerial vehicles do not need drivers and can be operated remotely and autonomously, are small in size, can realize various flight attitudes such as hovering, side flying and falling, and play an increasingly important role in application scenes where manual operations such as high-altitude shooting, military reconnaissance, high-altitude detection and agricultural application are risky or cannot be implemented due to the special performances of the unmanned aerial vehicles.
At present, the unmanned aerial vehicle receives signals transmitted by a remote controller through a central control device, and then drives a machine body to take off through rotation of screw propellers at two sides, and dangerous or inconvenient work is carried out through control of the remote controller.
But in the scheme, when the unmanned aerial vehicle is controlled on the ground to fly, the unmanned aerial vehicle is inconvenient to observe in some places and is easy to collide with other objects, so that the damage of the machine body is caused, and the normal flight of the unmanned aerial vehicle is influenced.
Disclosure of utility model
The utility model aims to provide an unmanned aerial vehicle capable of independently avoiding obstacle flight based on route planning, which solves the problem that when an operator is on the ground to control the unmanned aerial vehicle to fly, the unmanned aerial vehicle is inconvenient to observe in some places and is easy to collide with other objects, and the damage of a machine body is caused, so that the normal flight of the unmanned aerial vehicle is influenced.
In order to achieve the above purpose, the utility model provides an unmanned aerial vehicle based on route planning autonomous obstacle avoidance flight, which comprises a fuselage, a rotating motor, a propeller and a control center, wherein the rotating motor is fixedly connected with the fuselage and is positioned at one side of the fuselage, the propeller is fixedly connected with the output end of the rotating motor and is positioned at one side of the rotating motor, and the control center is fixedly connected with the fuselage and is positioned at one side of the fuselage and further comprises an autonomous avoidance assembly; the automatic avoidance assembly comprises an ultrasonic sensing device, a fixing piece, a camera, a supporting rod and a baffle, wherein the ultrasonic sensing device is fixedly connected with the machine body and is positioned on one side of the machine body, the fixing piece is fixedly connected with the machine body and is positioned on one side of the machine body, the camera is fixedly connected with the fixing piece and is positioned on one side of the fixing piece, the supporting rod is fixedly connected with the machine body and is positioned on one side of the machine body, and the baffle is fixedly connected with the supporting rod and is positioned on one side of the supporting rod.
The automatic avoidance assembly further comprises an elastic block, wherein the elastic block is fixedly connected with the baffle and is located on one side of the baffle.
The unmanned aerial vehicle based on the route planning autonomous obstacle avoidance flight further comprises a telescopic antenna, wherein the telescopic antenna is fixedly connected with the body and is located on one side of the body.
The unmanned aerial vehicle based on the route planning autonomous obstacle avoidance flight further comprises a telescopic motor and a foot rest, wherein the telescopic motor is fixedly connected with the body and is positioned on one side of the body, and the foot rest is fixedly connected with the output end of the telescopic motor and is positioned on one side of the telescopic motor.
The unmanned aerial vehicle based on the route planning autonomous obstacle avoidance flight further comprises a storage battery pack, wherein the storage battery pack is fixedly connected with the body and is located on one side of the body.
The unmanned aerial vehicle based on the route planning autonomous obstacle avoidance flight further comprises a night indicator lamp, wherein the night indicator lamp is fixedly connected with the body and is located on one side of the body.
According to the unmanned aerial vehicle capable of independently avoiding barrier flight based on route planning, the control center is arranged in the fuselage, the control center is protected, the four directions of the fuselage are prolonged to form flight wings, the rotating motor is arranged in the control center, the output end of the rotating motor continuously drives the propeller to rotate, so that the whole fuselage is driven to fly, the stability of the flight can be ensured through rotation in four directions, the ultrasonic wave sensing device can send out ultrasonic waves forward in the flight process, the ultrasonic waves return after the ultrasonic waves touch objects, and then the ultrasonic waves are transmitted to the remote controller according to returned signals, meanwhile, the camera arranged at the bottom of the fuselage is spherical, so that general visual field information at the bottom can be obtained, the partial visual field and the ultrasonic signals are synchronously returned to the remote controller, reasonable barriers are carried out through the information, the control center can control the direction change of the fuselage in advance when the control center is very close to the barriers, the outside of the wing supports the baffle to avoid the barrier to directly collide with the unmanned aerial vehicle, and damage caused by the barrier is avoided.
Drawings
In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below.
Fig. 1 is a schematic overall structure of a first embodiment of the present utility model.
Fig. 2 is a bottom view of the entirety of the first embodiment of the present utility model.
Fig. 3 is an overall cross-sectional view of a first embodiment of the present utility model.
Fig. 4 is a schematic overall structure of a second embodiment of the present utility model.
101-Fuselage, 102-rotating electrical machines, 103-screw, 104-control center, 105-ultrasonic sensing device, 106-mounting, 107-camera, 108-bracing piece, 109-baffle, 110-elastic block, 111-telescopic antenna, 112-telescopic motor, 113-foot rest, 114-storage battery, 201-night pilot lamp.
Detailed Description
The first embodiment of the application is as follows:
Referring to fig. 1-3, fig. 1 is a schematic overall structure of a first embodiment of the present utility model, fig. 2 is a bottom overall view of the first embodiment of the present utility model, and fig. 3 is a cross-sectional overall view of the first embodiment of the present utility model.
The utility model provides an unmanned aerial vehicle based on route planning autonomous obstacle avoidance flight, which comprises a machine body 101, a rotating motor 102, a propeller 103, a control center 104, a telescopic motor 112, a foot rest 113, a storage battery pack 114, a telescopic antenna 111 and an autonomous avoidance assembly, wherein the autonomous avoidance assembly comprises an ultrasonic sensing device 105, a fixing piece 106, a camera 107, a supporting rod 108, a baffle 109 and an elastic block 110.
For this embodiment, the rotating motor 102 is fixedly connected to the body 101, and is located at one side of the body 101, the propeller 103 is fixedly connected to an output end of the rotating motor 102, and is located at one side of the rotating motor 102, the control center 104 is fixedly connected to the body 101, and is located at one side of the body 101, the control center 104 is installed inside the body 101, the control center 104 is protected, the four directions of the body 101 are extended to form a flying wing, the rotating motor 102 is installed therein, the output end of the rotating motor 102 continuously drives the propeller 103 to rotate, so that the whole body 101 is driven to fly, and the flying stability can be ensured through the rotation in four directions.
The ultrasonic sensing device 105 is fixedly connected with the machine body 101 and is located on one side of the machine body 101, the fixing piece 106 is fixedly connected with the machine body 101 and is located on one side of the machine body 101, the camera 107 is fixedly connected with the fixing piece 106 and is located on one side of the fixing piece 106, the supporting rod 108 is fixedly connected with the machine body 101 and is located on one side of the machine body 101, the baffle 109 is fixedly connected with the supporting rod 108 and is located on one side of the supporting rod 108, in the flying process, the ultrasonic sensing device 105 emits ultrasonic waves forwards, the ultrasonic waves return after hitting an object, then the ultrasonic waves are transmitted to the remote controller according to returned signals, meanwhile, the camera 107 installed at the bottom of the machine body 101 is spherical, the general view information of the bottom can be obtained, the partial view and the ultrasonic signals are synchronously returned to the remote controller, the control center 104 can control the direction change of the machine body 101 through reasonable obstacle avoidance through the information, the outside of the supporting rod 108 is used for directly supporting the machine body 101 to avoid the obstacle avoidance caused by the direct collision of the baffle 109.
Secondly, the elastic block 110 is fixedly connected with the baffle 109 and is located at one side of the baffle 109, the elastic block 110 is mounted on the surface of the baffle 109, when the emergency is avoided, the baffle 109 collides with an obstacle, and the elastic block 110 can buffer to avoid the obstacle of the control center 104 caused by overlarge collision.
Simultaneously, telescopic antenna 111 with fuselage 101 fixed connection, and be located one side of fuselage 101, telescopic antenna 111 can contract when not taking off and be convenient for accomodate, will before taking off telescopic antenna 111 is elongated, through telescopic antenna 111 strengthens the transmission of information, guarantees that the transmission of information is rapid, thereby lets the operator can make the reaction faster and avoids unmanned aerial vehicle to hit the barrier.
In addition, the telescopic motor 112 is fixedly connected with the machine body 101 and is located at one side of the machine body 101, the foot rest 113 is fixedly connected with the output end of the telescopic motor 112 and is located at one side of the telescopic motor 112, when taking off, the output end of the telescopic motor 112 rotates, the foot rest 113 is driven along with the rotation of the telescopic motor 112 to drive the foot rest 113 to shrink inwards to ensure the flatness of the bottom, the foot rest 113 is prevented from influencing the visual field acquisition of the camera 107 in the middle of flight, meanwhile, the foot rest 113 is easy to collide with an obstacle, when the unmanned aerial vehicle stops flying in falling, the output end of the telescopic motor 112 reverses to enable the foot rest 113 to fall down, and the unmanned aerial vehicle is convenient to buffer in the falling to the ground.
Secondly, the storage battery 114 is fixedly connected with the body 101 and is located at one side of the body 101, the storage battery 114 is provided as electric quantity of the whole unmanned aerial vehicle, the storage battery 114 is not a disposable battery, and the storage battery can be recharged through a charging port to store and ensure electric quantity replenishment during flying.
When the utility model is used, the control center 104 is arranged in the fuselage 101, the control center 104 is protected, the four directions of the fuselage 101 are prolonged to form flying wings, the rotating motor 102 is arranged in the flying wings, the telescopic antenna 111 is pulled out before taking off to improve the transmitted signal, the output end of the rotating motor 102 continuously drives the propeller 103 to rotate, thereby driving the whole fuselage 101 to fly, the output end of the rotating motor 102 rotates to retract the foot rest 113, the high-frequency rotation of the propeller 103 in four directions can ensure more stable flying, the ultrasonic wave sensing device 105 can send out ultrasonic waves forward in the flying process, the ultrasonic waves return after touching objects, then the ultrasonic waves are transmitted to the remote controller according to the returned signals, meanwhile, the camera 107 arranged at the bottom of the fuselage 101 is spherical, the common visual field information at the bottom can be obtained, the partial visual field and the ultrasonic signals are synchronously returned to the remote controller, reasonable obstacles are carried out through the information, the control center 104 can control the fuselage to rotate at first when the output end of the rotating motor 102 is very close to the obstacles, the external side of the fuselage is prevented from being damaged by the elastic baffle plate 109, and the outer surface of the fuselage is prevented from being damaged by the elastic baffle plate 109 when the aircraft is in the collision with the outer surface of the fuselage 101.
The second embodiment of the application is as follows:
Referring to fig. 4 on the basis of the first embodiment, fig. 4 is a schematic overall structure of a second embodiment of the present utility model, and the unmanned aerial vehicle based on the autonomous obstacle avoidance flight by route planning further includes a night indicator 201.
For this embodiment, the night indicator 201 is fixedly connected with the body 101, and is located on one side of the body 101, and when flying at night, the night indicator 201 may flash with lights of different colors, so as to ensure that the position and the flight track of the unmanned aerial vehicle can be seen clearly.
When the utility model is used, the control center 104 is arranged in the fuselage 101, the control center 104 is protected, the four directions of the fuselage 101 are prolonged to form flying wings, the rotating motor 102 is arranged in the flying wings, the telescopic antenna 111 is pulled out before taking off to improve the transmitted signal, the night indicator 201 is opened, the unmanned aerial vehicle is guaranteed to flash and transmit position signals during flying, the propeller 103 is continuously driven to rotate through the output end of the rotating motor 102, the whole fuselage 101 is driven to fly, the foot rest 113 is rotated and retracted through the output end of the rotating motor 102, the ultrasonic wave sensing device 105 can send out ultrasonic waves forwards during flying, the ultrasonic wave returns after touching an object, then the ultrasonic wave is transmitted to the remote controller according to the returned signal, meanwhile, the camera 107 arranged at the bottom of the fuselage 101 is spherical, the common visual field information can be obtained, the common visual field information of the bottom is synchronously returned to the remote controller with the ultrasonic wave signal, the ultrasonic wave is reasonably used for carrying out obstacle avoidance, the control center 104 is controlled to avoid the bump on the outer surface of the fuselage 101, and the aircraft is prevented from being damaged by the bump on the outer surface of the fuselage 109 when the aircraft is in the front of the aircraft, the aircraft is prevented from being damaged by the bump on the outer surface of the damper 109, and the aircraft is prevented from being damaged by the bump on the front of the aircraft 101 due to the control center 101.
The foregoing disclosure is only illustrative of one or more preferred embodiments of the present application, and it is not intended to limit the scope of the claims hereof, as persons of ordinary skill in the art will understand that all or part of the processes for practicing the embodiments described herein may be practiced with equivalent variations in the claims, which are within the scope of the application.
Claims (6)
1. An unmanned aerial vehicle based on route planning autonomous obstacle avoidance flight comprises a body, a rotating motor, a propeller and a control center, wherein the rotating motor is fixedly connected with the body and positioned on one side of the body, the propeller is fixedly connected with the output end of the rotating motor and positioned on one side of the rotating motor, the control center is fixedly connected with the body and positioned on one side of the body,
The system also comprises an autonomous avoidance assembly;
The automatic avoidance assembly comprises an ultrasonic sensing device, a fixing piece, a camera, a supporting rod and a baffle, wherein the ultrasonic sensing device is fixedly connected with the machine body and is positioned on one side of the machine body, the fixing piece is fixedly connected with the machine body and is positioned on one side of the machine body, the camera is fixedly connected with the fixing piece and is positioned on one side of the fixing piece, the supporting rod is fixedly connected with the machine body and is positioned on one side of the machine body, and the baffle is fixedly connected with the supporting rod and is positioned on one side of the supporting rod.
2. An unmanned aerial vehicle for autonomous obstacle avoidance flight based on route planning as claimed in claim 1,
The autonomous avoidance assembly further comprises an elastic block, wherein the elastic block is fixedly connected with the baffle and is located on one side of the baffle.
3. An unmanned aerial vehicle for autonomous obstacle avoidance flight based on route planning as claimed in claim 1,
Unmanned aerial vehicle based on unmanned aerial vehicle of obstacle avoidance flight independently of route planning still includes flexible antenna, flexible antenna with fuselage fixed connection, and be located one side of fuselage.
4. An unmanned aerial vehicle for autonomous obstacle avoidance flight based on route planning as claimed in claim 1,
Unmanned aerial vehicle based on unmanned aerial vehicle of obstacle avoidance flight independently of route planning still includes flexible motor and foot rest, flexible motor with fuselage fixed connection is located one side of fuselage, the foot rest with flexible motor's output fixed connection, and be located one side of flexible motor.
5. An unmanned aerial vehicle for autonomous obstacle avoidance flight based on route planning as claimed in claim 1,
Unmanned aerial vehicle based on unmanned aerial vehicle of obstacle avoidance flight independently of route planning still includes storage battery, storage battery with fuselage fixed connection, and be located one side of fuselage.
6. An unmanned aerial vehicle for autonomous obstacle avoidance flight based on route planning as claimed in claim 1,
Unmanned aerial vehicle based on unmanned aerial vehicle of obstacle avoidance flight independently of route planning still includes night pilot lamp, night pilot lamp with fuselage fixed connection, and be located one side of fuselage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202323089228.6U CN220933393U (en) | 2023-11-16 | 2023-11-16 | Unmanned aerial vehicle based on autonomous obstacle avoidance flight of route planning |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202323089228.6U CN220933393U (en) | 2023-11-16 | 2023-11-16 | Unmanned aerial vehicle based on autonomous obstacle avoidance flight of route planning |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220933393U true CN220933393U (en) | 2024-05-10 |
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ID=90966244
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202323089228.6U Active CN220933393U (en) | 2023-11-16 | 2023-11-16 | Unmanned aerial vehicle based on autonomous obstacle avoidance flight of route planning |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220933393U (en) |
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2023
- 2023-11-16 CN CN202323089228.6U patent/CN220933393U/en active Active
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