Patents
Literature
Patsnap Copilot is an intelligent assistant for R&D personnel, combined with Patent DNA, to facilitate innovative research.
Patsnap Copilot

40results about How to "Realize autonomous flight" patented technology

Multi-rotor type unmanned aircraft system with fire detecting function

The invention provides a multi-rotor type unmanned aircraft system with a fire detecting function. Six engine arms and a frame form a body frame of the multi-rotor type unmanned aircraft system; a motor and an electronic speed regulator are connected with each other to control the rotation speed of propeller blades; a landing gear is used for an aircraft to stably land during landing; an unmanned aircraft flight control system is used for controlling stable postures of the aircraft; a sensor is connected with the unmanned aircraft flight control system; a small-sized control computer is connected with laser distance measuring sensors through communication; a processed signal is input into the unmanned aircraft flight control system to control three-dimensional positions and postures of the aircraft indoors; high-definition cameras are connected with an image transmitting device to collect video images of environment; and the image transmitting device is used for transmitting a video image signal to a ground station device so as to realize real-time observation. The multi-rotor type unmanned aircraft system with the fire detecting function, provided by the invention, is advantaged in that the multi-rotor type unmanned aircraft system can autonomously fly under a complicated environment, automatically detect fires in real time, automatically avoid obstacles and protect personal safety; remote monitoring and remote real-time communication are realized; data can be saved and replayed and so on.
Owner:湖北省机电研究设计院股份公司

System and method for multi-power integrated flight control applied in micro air vehicle

InactiveCN105468009AReduce loadImprove Powertrain EfficiencyAttitude controlFlight control modesMicro air vehicle
The invention provides a system and method for multi-power integrated flight control applied in a micro air vehicle. The system comprises a flight control computer, a flight parameter sensor, a PID controller, a yaw propeller power system, a posture propeller power system and a main propeller power system, wherein an output end of the flight parameter sensor is connected to an input end of the flight control computer, and an output end of the flight control computer is separately connected to the yaw propeller power system, the posture propeller power system and main propeller power system by the PID controller. The system and method provided by the invention have the advantages that (1) a layout manner of a main propeller, a posture propeller and a yaw propeller is applied, so that a load of the posture propeller can be effectively reduced during a flight course, efficiency of a power system of the air vehicle can be effectively increased, and flight duration of the air vehicle can be increased; and (2) integrated control is carried out to the multiple sets of power systems of the air vehicle, so that the problem that lift force of the main propeller of the air vehicle is unstable and the problem about reverse torque balance of the main propeller can be solved, and finally autonomous flight of the multi-rotor air vehicle with the new layout can be realized.
Owner:NORTHWESTERN POLYTECHNICAL UNIV

Power line patrol unmanned aerial vehicle wireless charging relay station, charging flight control system and method

The invention discloses a power line patrol unmanned aerial vehicle wireless charging relay station, a charging flight control system and a charging flight control method. The unmanned aerial vehiclewireless charging relay station comprises: a charging platform which is arranged on a power transmission tower and is provided with a wireless charging area for charging an unmanned aerial vehicle; anelectromagnetic locking device, wherein the electromagnetic locking device is used for generating magnetic attraction force to attract the unmanned aerial vehicle onto the charging platform when theunmanned aerial vehicle is charged, and generating magnetic repulsive force to enable the unmanned aerial vehicle to catapult and take off when the unmanned aerial vehicle takes off; a clamping device, wherein the clamping device is used for clamping the unmanned aerial vehicle in the wireless charging area in the transverse direction and the longitudinal direction; a CT power taking device, wherein the CT power taking device takes power from the power transmission line and supplies power to the charging platform, the electromagnetic locking device and the clamping device; and a controller. wherein the controller is connected with the transmitting end of the wireless charging system, the electromagnetic locking device and the clamping device in the wireless charging area. And the unmannedaerial vehicle automatically searches the nearest wireless charging relay station for electric energy supply, and long-distance uninterrupted autonomous line patrol is carried out.
Owner:WUHAN UNIV

Unmanned aerial vehicle inspection control method and system, storage medium, program and terminal

The invention belongs to the technical field of driving safety monitoring, and discloses an unmanned aerial vehicle inspection control method and system, a storage medium, a program and a terminal. The method comprises the following steps of editing an unmanned aerial vehicle flight route, identifying an image by the program and adjusting a pod angle to enable an expressway to be located in the center of a picture; automatically identifying lane lines and objects in the expressway, and analyzing to find illegal driving behaviors and road condition potential safety hazards in the expressway; automatically capturing license plates of the illegal driving behaviors with evidences reserved, and giving a voice prompt for the road condition potential safety hazards; and displaying the expresswaycondition and illegal driving behavior information in real time. The program is adopted for control in the whole process, and an intelligent identification control algorithm is combined, so that a traditional manual inspection mode is completely replaced; the inspection hidden danger is reduced; manpower, material resources and financial resources are saved; the inspection efficiency is improved;and more illegal events can be handled. Meanwhile, the defect that a fixed blind area exists in traffic block port equipment monitoring is overcome.
Owner:西安智文琛软件有限公司 +1

Fixed-wing unmanned aerial vehicle cluster control collision avoidance method and device based on deep reinforcement learning

The invention discloses a fixed-wing unmanned aerial vehicle cluster control collision avoidance method and device based on deep reinforcement learning. The method comprises the steps of S1, establishing an unmanned aerial vehicle kinematic model and D3QN, updating network parameters by using historical interaction data in the interaction process of each wing plane and the environment; training toform a D3QN model, constructing a joint state between the wing planes and a lead plane according to the environment state in the interaction process, performing situation assessment construction to obtain a local map, and inputting the local map into the D3QN model to obtain control instruction output of each wing plane; S2, obtaining state information in real time by each wing plane to form a joint state between the current wing plane and the lead plane, carrying out situation assessment in real time to construct a local map, and inputting the joint state constructed in real time and the local map into the D3QN network model to obtain a control instruction of each wing plane. The method has the advantages that the implementation method is simple, the expandability is good, cluster control over the fixed-wing unmanned aerial vehicles can be achieved, and meanwhile, collision is avoided.
Owner:NAT UNIV OF DEFENSE TECH

Unmanned aerial vehicle bionic intelligent obstacle-avoiding method based on light streams

The invention discloses an unmanned aerial vehicle bionic intelligent obstacle-avoiding method based on light streams and belongs to the field of artificial intelligence and computer vision. Obstacle-avoiding flight of an unmanned aerial vehicle is realized through combination of software and hardware. The method comprises the specific steps that an image sequence is captured through a monocular camera carried on the unmanned aerial vehicle, an LK (Lucas Kanade) method is used for calculating a light stream field according to a front frame image and a rear frame image, and noise light streams are filtered; each image is divided into an edge, a left middle part and a right middle part, and whether large obstacles exist on the left side and the right side or not is judged based on an SVM classifier; the sum of TTC in all columns is calculated, free sections and obstacle sections are calibrated and interpolated, and a maximum free communicating section is obtained; a translation amount and a rotation amount are obtained in combination with a left and right light stream balancing strategy, and therefore the unmanned aerial vehicle is controlled to fly avoiding obstacles. By means of the method, real-time obstacle-avoiding flight of the unmanned aerial vehicle in an unknown disordered environment can be realized.
Owner:ANHUI EYEVOLUTION TECH CO LTD

Autonomous flight path planning method for small-sized unmanned aerial vehicle

The invention discloses an autonomous flight path planning method for a small-sized unmanned aerial vehicle. The method comprises the following steps that: S1, GPS positioning is carried out: the GPSof a four-axis aircraft is adopted to locate the position of the small-sized unmanned aerial vehicle; S2, an improved A-Star algorithm is used as a flight path planning algorithm to achieve the flightpath tracking of the small-sized unmanned aerial vehicle; S3, an ant colony evolution algorithm is adopted to optimize feasible flight paths: a flight path calculated by the improved A-Star algorithmin the S2 is inputted to the ant colony algorithm, and the ant colony algorithm optimizes the feasible flight paths and calculates a shortest flight path; and S4, post-processing is performed on an optimal flight path: all flight path points on the same line are summarized into a straight line segment containing a head end point and a tail end point. A traditional small-sized unmanned aerial vehicle is controlled by a remote control device, the movement range of the small-sized unmanned aerial vehicle is easily limited to the sight distance range of a controller, and as a result, the autonomous flight of the small-sized unmanned aerial vehicle cannot be realized, and the small-sized unmanned aerial vehicle cannot have a wider movement range, while, with the method of the invention adopted, the above problem can be solved.
Owner:长春市维伲机器人科技有限责任公司

Dedicated flight control system for multi-rotor unmanned aerial vehicle

The invention relates to a dedicated flight control system for a multi-rotor unmanned aerial vehicle. The system comprises a multi-rotor unmanned aerial on which a liquid spraying device is carried; and ground liquid supply equipment connected with the multi-rotor unmanned aerial vehicle through a transfusion hose and used for supplying liquid, required by the liquid spraying device in work, for the multi-rotor unmanned aerial vehicle in the work process of the multi-rotor unmanned aerial vehicle; the system further comprises ground power supply equipment connected with the multi-rotor unmanned aerial vehicle through a power supply line and used for supplying electric energy for the multi-rotor unmanned aerial vehicle in the work process of the multi-rotor unmanned aerial vehicle; the multi-rotor unmanned aerial vehicle comprises an unmanned aerial vehicle comprehensive management module, a height control submodule, an airway navigation control submodule, and a spraying control submodule. The flight control for driving the multi-rotor unmanned aerial vehicle is realized, the plant protection work can be performed along a preset flight airway, the system can deal with various complex terrains, relieve the labor intensity of a remote operator, and avoid missing spraying or re-spraying of the pesticide.
Owner:智飞智能装备科技东台有限公司

Indoor unmanned aerial vehicle, control method thereof and computer readable storage medium

The invention discloses an indoor unmanned aerial vehicle, a control method thereof and a computer readable storage medium, and the method comprises the steps: enabling the unmanned aerial vehicle toshoot a picture in real time, recognizing a symbolic object in the picture, and estimating the position of the unmanned aerial vehicle in a map through employing the recognized symbolic object as a reference object; taking the estimated position as the position of the unmanned aerial vehicle to plan a path from the position of the unmanned aerial vehicle to an end point, and controlling the unmanned aerial vehicle to fly based on the planned path. The method includes: shooting a picture in real time and identifying the picture in a flight process, estimating the position of the unmanned aerialvehicle in a map by taking a newly identified symbolic object as a reference object when the symbolic object is identified, correcting the position of the unmanned aerial vehicle based on the estimated position, and planning a path from the position of the unmanned aerial vehicle to an end point again after the position is corrected. According to the invention, autonomous positioning, path planning and autonomous flight can be achieved; furthermore, the invention also provides a traffic sign recognition method based on a deep learning framework, and the method can help to correct the positionof the unmanned aerial vehicle and perfect and update a map.
Owner:宁波图灵奇点智能科技有限公司

Small unmanned helicopter flight control computer system

The invention relates to a small unmanned helicopter flight control computer system. The system comprises a communication processor, a programmable gate array, a power module, a clock module, a wireless communication module, an electronic compass, a GPS, an ultrasonic sensor, a debugging serial port, an Ethernet port, a remote-control receiver, a steering engine, a height gauge, a gyroscope and anaccelerometer, wherein the power module is connected with the communication processor and the programmable gate array; the clock module is connected with the communication processor and the programmable gate array; the wireless communication module, the electronic compass, the GPS, the ultrasonic sensor, the debugging serial port and the Ethernet port are respectively connected with the communication processor; the remote-control receiver, the steering engine, the height gauge, the gyroscope and the accelerometer are respectively connected with the programmable gate array; and the steering engine is connected with an unmanned aerial vehicle. The small unmanned helicopter flight control computer system has the characteristics of being small in volume, compact in structure, low in power consumption and strong in processing ability, and is capable of successfully realizing autonomous flight of small unmanned helicopters on the basis.
Owner:成都纵海科技有限公司

Inflatable water surface take-off and landing parafoil

ActiveCN112644706ARealize automatic stretch functionTakeoff and landingWaterborne vesselsMicrolight aircraftsMarine engineeringStructural engineering
The invention discloses an inflatable water surface take-off and landing parafoil which comprises a parafoil body, an inflation and deflation device, a folding and unfolding device, a load cabin, a left parafoil rope and a right parafoil rope, wherein the left parafoil rope and the right parafoil rope are connected with the parafoil body and the load cabin. The load cabin has buoyancy and can float on the water surface, so that the parafoil can take off and land on the water surface. The parafoil comprises three or more transverse inflatable parafoil bags and longitudinal inflatable parafoil bags arranged at the two ends of the transverse inflatable parafoil bags and used for connecting the transverse inflatable parafoil bags into a whole. The inflatable parafoil bags are communicated with one another; the electric inflation / deflation pump inflates / deflates the parafoil through the inflatable parafoil umbilical cord; the two longitudinal ends of the interior of each longitudinal inflatable parafoil bag are each connected with a guide rope, the guide ropes are wound around a winding drum in a sealed cabin of a winder after being subjected to reversing traction of a guide device, and folding and unfolding of the parafoil are achieved through folding and unfolding of the winder on the guide ropes.
Owner:深圳市百川融创科技有限公司

UAV (Unmanned Aerial Vehicle) plant protection operation system and method

The invention discloses an UAV (Unmanned Aerial Vehicle) plant protection operation system and method and relates to the field of UAVs. The UAV plant protection operation system comprises a ground base station, a surveying and mapping UAV, a ground server, a ground control station and an operation UAV; the ground base station is in communication connection with the surveying and mapping UAV and the operation UAV respectively; the surveying and mapping UAV is in communication connection with the ground server; the ground server is in communication connection with the ground control station; theground control station is in communication connection with the operation UAV. The ground base station is used for providing satellite positioning signals for the surveying and mapping UAV and the operation UAV; the surveying and mapping UAV is used for collecting and transmitting information to the ground server; the ground server is used for generating and transmitting a reference operation pathto the ground control station; the ground control station is used for generating and uploading an actual operation path to the operation UAV; the operation UAV performs plant protection operation according to the actual operation path. The UAV plant protection operation system and method have the advantage that the degrees of intellectualization and autonomy of the plant protection operation areimproved.
Owner:濉溪淮匠机械设备有限责任公司

A miniature flapping-wing robot with autonomous power supply

The invention discloses a micro flapping wing robot with independent power supply, which comprises a fuselage support frame, a wing, a piezoelectric driver, a high-voltage pulse power supply module, awireless communication module and a transmission amplification mechanism. The micro flapping wing robot comprises an airframe support frame, a wing, a piezoelectric driver, a high-voltage pulse powersupply module, a wireless communication module and a transmission amplification mechanism. Piezoelectric ceramic bimorph is used as piezoelectric actuator, piezoelectric ceramic bimorph drives wing through drive amplification mechanism. The high voltage pulse module outputs a high voltage pulse square wave signal. The wireless communication module receives the control signal from the ground and controls the output of the high voltage pulse module. In flight, piezoelectric ceramic bimorph acts as piezoelectric actuator, inputs high voltage pulse signal, amplifies and converts the vibration ofpiezoelectric ceramic bimorph into wing vibration frequency and duty cycle through transmission amplification mechanism, and then controls the amplitude and angle of flutter of two wings, realizes forward, backward, steering, hovering and other flight postures. The robot can fly autonomously for a long distance because of its power supply system. Flight control of robot is realized by wireless communication, and the robot has strong adaptability to bad weather.
Owner:ZHEJIANG UNIV
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products