CN212278237U - All-weather intelligent flight system of unmanned aerial vehicle - Google Patents
All-weather intelligent flight system of unmanned aerial vehicle Download PDFInfo
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- CN212278237U CN212278237U CN202020905783.9U CN202020905783U CN212278237U CN 212278237 U CN212278237 U CN 212278237U CN 202020905783 U CN202020905783 U CN 202020905783U CN 212278237 U CN212278237 U CN 212278237U
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Abstract
The utility model discloses a belong to the technical field of unmanned aerial vehicle, specifically be an all-weather intelligent flight system of unmanned aerial vehicle, include: the system comprises an airborne control center, a remote control center and a remote control center, wherein the airborne control center is integrated on an unmanned aerial vehicle and is used for controlling the flight mode, flight monitoring and landing of the unmanned aerial vehicle; the flight control system is electrically connected with the airborne control center, the airborne control center outputs a control instruction to the flight control system, and the flight control system controls the flight mode of the unmanned aerial vehicle according to the control instruction; the airborne monitoring system can remotely acquire state information of the unmanned aerial vehicle and control the unmanned aerial vehicle in a data transmission and control mode through the communication module between the airborne control center and the ground control base station; through the setting of platform monitored control system that rises and falls, the use of cooperation scanning camera can be to the platform control that rises and falls to take off and descend that can be better, raise the efficiency.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is an all-weather intelligent flight system of unmanned aerial vehicle.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer.
Drones tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than are manned aircraft. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology.
After the unmanned aerial vehicle flies out on duty, ground is difficult to control in time to unmanned aerial vehicle's state, and unmanned aerial vehicle need stop on the platform that rises and falls usually after falling back, and the ground personnel are difficult to control the state of whether the platform that rises and falls carries the aircraft.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an all-weather intelligent flight system of unmanned aerial vehicle to solve the unmanned aerial vehicle that provides in the above-mentioned background art and fly away on duty after, ground is difficult to in time to unmanned aerial vehicle's state and controls, and unmanned aerial vehicle need stop after falling back usually on the platform that rises and falls, and the ground personnel are difficult to the problem of controlling the state of the platform that rises and falls whether the aircraft.
In order to achieve the above object, the utility model provides a following technical scheme: an all-weather intelligent flight system of an unmanned aerial vehicle, comprising:
the system comprises an airborne control center, a remote control center and a remote control center, wherein the airborne control center is integrated on an unmanned aerial vehicle and is used for controlling the flight mode, flight monitoring and landing of the unmanned aerial vehicle;
the flight control system is electrically connected with the airborne control center, the airborne control center outputs a control instruction to the flight control system, and the flight control system controls the flight mode of the unmanned aerial vehicle according to the control instruction;
the system comprises an airborne monitoring system, a speed detection module, a positioning module and a distance detection module, wherein the airborne monitoring system is electrically connected with an airborne control center and is used for monitoring the self equipment and the flight state of the unmanned aerial vehicle, and the airborne monitoring system comprises a temperature detection module, an electric quantity detection module, a speed detection module, a positioning module and a distance detection module;
the scanning camera is electrically connected with the airborne control center, and is used for scanning and identifying an object and lifting and descending an identification lifting platform;
the communication module is electrically connected with the airborne control center and is used for receiving and transmitting data information by the unmanned aerial vehicle;
the ground control base station is connected with the communication module, outputs a control instruction to the airborne control center through the communication module, controls the flight mode of the unmanned aerial vehicle through the airborne control center, and acquires the flight state and the energy use state receiving of the flying unmanned aerial vehicle of the unmanned aerial vehicle through the communication module;
the utility model provides a landing platform monitored control system, landing platform monitored control system and ground control basic station electric connection, on placing unmanned aerial vehicle's the platform that rises and falls on the landing platform monitored control system, the platform monitored control system that rises and falls whether have unmanned aerial vehicle to monitor and export monitoring information to ground control basic station on the platform that rises and falls, ground control basic station output instruction to airborne control center to control through airborne control center control this unmanned aerial vehicle berth on the platform that does not have unmanned aerial vehicle that rises and falls.
Preferably, the flight control system comprises a flight speed control module, a flight angle control module and a flight direction control module, and the flight speed control module and the flight direction control module output power mechanisms for controlling the unmanned aerial vehicle.
Preferably, the control mode of the flight speed control module is to control the output power of a power mechanism of the unmanned aerial vehicle.
Preferably, the control modes of the flight direction control module are all differences generated by controlling the power mechanisms on two sides of the unmanned aerial vehicle to output power.
Preferably, the power mechanism outputs power in a manner of increasing the power mechanism output power on one side or decreasing the power mechanism output power on the other side.
Preferably, the landing platform monitoring system comprises a gravity sensor and a data transmission bus, the gravity sensor is arranged on the landing platform, the gravity value range detected by the gravity sensor in the state of having the unmanned aerial vehicle and not having the unmanned aerial vehicle on the landing platform is in two stages, and the gravity sensor outputs the detected gravity value to the ground control base station through the data transmission bus.
Compared with the prior art, the beneficial effects of the utility model are that:
1) the airborne control center and the ground control base station can remotely acquire state information of the unmanned aerial vehicle and control the unmanned aerial vehicle in a data transmission and control mode through the communication module;
2) through the setting of platform monitored control system that rises and falls, the use of cooperation scanning camera can be to the platform control that rises and falls to take off and descend that can be better, raise the efficiency.
Drawings
FIG. 1 is a logic block diagram of the system of the present invention;
fig. 2 is the utility model discloses an unmanned aerial vehicle and landing platform's schematic diagram.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
In the description of the present invention, it is to be understood that the terms "upper", "lower", "front", "rear", "left", "right", "top", "bottom", "inner", "outer", and the like 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, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention.
Example (b):
referring to fig. 1-2, the present invention provides a technical solution: an all-weather intelligent flight system of an unmanned aerial vehicle, comprising:
the system comprises an airborne control center, a remote control center and a remote control center, wherein the airborne control center is integrated on an unmanned aerial vehicle and is used for controlling the flight mode, flight monitoring and landing of the unmanned aerial vehicle;
the flight control system is electrically connected with the airborne control center, the airborne control center outputs a control instruction to the flight control system, and the flight control system controls the flight mode of the unmanned aerial vehicle according to the control instruction;
the system comprises an airborne monitoring system, a speed detection module, a positioning module and a distance detection module, wherein the airborne monitoring system is electrically connected with an airborne control center and is used for monitoring the self equipment and the flight state of the unmanned aerial vehicle, and the airborne monitoring system comprises a temperature detection module, an electric quantity detection module, a speed detection module, a positioning module and a distance detection module;
the scanning camera is electrically connected with the airborne control center, and is used for scanning and identifying an object and lifting and descending an identification lifting platform;
the communication module is electrically connected with the airborne control center and is used for receiving and transmitting data information by the unmanned aerial vehicle;
the ground control base station is connected with the communication module, outputs a control instruction to the airborne control center through the communication module, controls the flight mode of the unmanned aerial vehicle through the airborne control center, and acquires the flight state and the energy use state receiving of the flying unmanned aerial vehicle of the unmanned aerial vehicle through the communication module;
the utility model provides a landing platform monitored control system, landing platform monitored control system and ground control basic station electric connection, on placing unmanned aerial vehicle's the platform that rises and falls on the landing platform monitored control system, the platform monitored control system that rises and falls whether have unmanned aerial vehicle to monitor and export monitoring information to ground control basic station on the platform that rises and falls, ground control basic station output instruction to airborne control center to control through airborne control center control this unmanned aerial vehicle berth on the platform that does not have unmanned aerial vehicle that rises and falls.
Further, flight control system includes airspeed control module, flight angle control module and flight direction control module, airspeed control module and flight direction control module output control unmanned aerial vehicle's power unit.
Furthermore, the control mode of the flight speed control module is to control the output power of a power mechanism of the unmanned aerial vehicle.
Furthermore, the control modes of the flight direction control module are all differences generated by controlling the power mechanisms on two sides of the unmanned aerial vehicle to output power.
Further, the power mechanism output power is differentiated by increasing the power mechanism output power on one side or decreasing the power mechanism output power on the other side.
Furthermore, the lifting platform monitoring system comprises a gravity sensor and a data transmission bus, the gravity sensor is arranged on the lifting platform, a gravity value range detected by the gravity sensor in a state that the unmanned aerial vehicle is arranged on the lifting platform and the unmanned aerial vehicle is not arranged on the lifting platform is in two stages, and the gravity sensor outputs the detected gravity value to the ground control base station through the data transmission bus.
The airborne control center detects the electric energy state of the unmanned aerial vehicle and detects each electric device of the unmanned aerial vehicle, the unmanned aerial vehicle starts to take off when the takeoff standard is reached, the flight control system controls the flight direction, the flight speed and the like of the unmanned aerial vehicle in the flight process, and the airborne monitoring system monitors various data of the unmanned aerial vehicle in real time and outputs the data to the ground control base station through the communication module;
when landing is needed, the ground control base station monitors the state of each landing platform through the landing platform monitoring system, and commands the unmanned aerial vehicle to the landing platform without the unmanned aerial vehicle, and the flight control system scans and identifies the landing platform through the scanning camera (by adopting the existing image identification technology, when the landing platform does not have the image information of the unmanned aerial vehicle, the landing platform does not have the unmanned aerial vehicle, when the landing platform has the image information of the unmanned aerial vehicle, the landing platform has the unmanned aerial vehicle), further confirming that when the landing platform has the unmanned aerial vehicle, the ground control base station redistributes the landing platform to the unmanned aerial vehicle to be landed; when there is no unmanned aerial vehicle on the landing platform, the unmanned aerial vehicle about to land continues to descend until it lands on the landing platform.
As shown in fig. 2, unmanned aerial vehicle and the cooperation sketch map of the platform that rises and falls, unmanned aerial vehicle can take off and land under extreme climatic conditions, and the material that the weatherability is good is adopted to unmanned aerial vehicle's outside, like compound polyethylene material, at rainwater or hot weather, it can guarantee sufficient toughness and corrosion resistance.
Establish data contact between unmanned aerial vehicle and the platform that rises and falls, on the platform that rises and falls of arranging unmanned aerial vehicle in on the platform monitored control system that rises and falls, whether platform monitored control system that rises and falls has unmanned aerial vehicle to monitor information output to ground control basic station on to the platform that rises and falls, ground control basic station output instruction to airborne control center to control through airborne control center control this unmanned aerial vehicle stop on the platform that rises and falls that does not have unmanned aerial vehicle.
Having shown and described the basic principles and principal features of the invention and advantages thereof, it will be apparent to those skilled in the art that the invention is not limited to the details of the foregoing exemplary embodiments, but is capable of other specific forms without departing from the spirit or essential characteristics thereof; the present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein, and any reference signs in the claims are not intended to be construed as limiting the claim concerned.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (3)
1. An all-weather intelligent flight system of unmanned aerial vehicle, its characterized in that includes:
the system comprises an airborne control center, a remote control center and a remote control center, wherein the airborne control center is integrated on an unmanned aerial vehicle and is used for controlling the flight mode, flight monitoring and landing of the unmanned aerial vehicle;
the flight control system is electrically connected with the airborne control center, the airborne control center outputs a control instruction to the flight control system, and the flight control system controls the flight mode of the unmanned aerial vehicle according to the control instruction;
the system comprises an airborne monitoring system, a speed detection module, a positioning module and a distance detection module, wherein the airborne monitoring system is electrically connected with an airborne control center and is used for monitoring the self equipment and the flight state of the unmanned aerial vehicle, and the airborne monitoring system comprises a temperature detection module, an electric quantity detection module, a speed detection module, a positioning module and a distance detection module;
the scanning camera is electrically connected with the airborne control center, and is used for scanning and identifying an object and lifting and descending an identification lifting platform;
the communication module is electrically connected with the airborne control center and is used for receiving and transmitting data information by the unmanned aerial vehicle;
the ground control base station is connected with the communication module, outputs a control instruction to the airborne control center through the communication module, controls the flight mode of the unmanned aerial vehicle through the airborne control center, and acquires the flight state and the energy use state receiving of the flying unmanned aerial vehicle of the unmanned aerial vehicle through the communication module;
the utility model provides a landing platform monitored control system, landing platform monitored control system and ground control basic station electric connection, on placing unmanned aerial vehicle's the platform that rises and falls on the landing platform monitored control system, the platform monitored control system that rises and falls whether have unmanned aerial vehicle to monitor and export monitoring information to ground control basic station on the platform that rises and falls, ground control basic station output instruction to airborne control center to control through airborne control center control this unmanned aerial vehicle berth on the platform that does not have unmanned aerial vehicle that rises and falls.
2. The all-weather intelligent flight system of unmanned aerial vehicle as claimed in claim 1, wherein: the flight control system comprises a flight speed control module, a flight angle control module and a flight direction control module, wherein the flight speed control module and the flight direction control module output and control an unmanned aerial vehicle power mechanism.
3. The all-weather intelligent flight system of unmanned aerial vehicle as claimed in claim 1, wherein: the system comprises a landing platform monitoring system and a ground control base station, wherein the landing platform monitoring system comprises a gravity sensor and a data transmission bus, the gravity sensor is arranged on the landing platform, a gravity value range detected by the gravity sensor in an unmanned aerial vehicle state and a gravity value range detected by the gravity sensor in an unmanned aerial vehicle state are in two stages, and the gravity sensor outputs the detected gravity value to the ground control base station through the data transmission bus.
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| Application Number | Priority Date | Filing Date | Title |
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| CN202020905783.9U CN212278237U (en) | 2020-05-26 | 2020-05-26 | All-weather intelligent flight system of unmanned aerial vehicle |
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| CN202020905783.9U CN212278237U (en) | 2020-05-26 | 2020-05-26 | All-weather intelligent flight system of unmanned aerial vehicle |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111431591A (en) * | 2020-05-26 | 2020-07-17 | 南京森林警察学院 | All-weather intelligent flight system of unmanned aerial vehicle |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111431591A (en) * | 2020-05-26 | 2020-07-17 | 南京森林警察学院 | All-weather intelligent flight system of unmanned aerial vehicle |
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