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221results about How to "Effectively completed" patented technology

Intelligent control method of driverless vehicle tracking desired trajectory

The invention discloses an intelligent control method of a driverless vehicle tracking a desired trajectory. The method is characterized by comprising the following steps of: establishing a body coordinate system, and determining the position information of the vehicle; calculating a membership degree function of a road curvature characteristic according to a radian value, and defining a fuzzy rule to calculate a decision output speed; according to the distance the vehicle runs for 1.5-2.5 seconds, searching for the trajectory points larger than the distance and closest to the vehicle in the coordinate sequence of the desired trajectory; calculating the moving curvature of the vehicle according to an adaptive proportion-differential-integral control algorithm formula; and finally judging whether the target point of the current control cycle is the last point selected from the road point sequence; if so, outputting a signal to a brake servo control system to start the brake to slow down the vehicle; otherwise, outputting a voltage signal by a controller local area network module to keep and control the accelerator opening so that the vehicle continues proceeding. Through adoption of the intelligent control method, the driverless vehicle can realize a function of tracking the desired trajectory, and has certain adaptability to the change of the road curvature characteristic.
Owner:HEFEI INSTITUTES OF PHYSICAL SCIENCE - CHINESE ACAD OF SCI

Unmanned plane aerial photographing system and method of photographing accompanying aircraft

The invention discloses an unmanned plane aerial photographing system and method of a photographing accompanying aircraft, and belongs to the application field of unmanned planes. The system comprises a main flight aircraft and a flight accompanying unmanned plane carrying aerial photographing equipment. The system further comprises a positioning identification device and a synchronizer. The positioning identification device obtains position information of the main flight aircraft and the flight accompanying unmanned plane, and calculates and obtains a relative position relation between the main flight aircraft and the flight accompanying unmanned plane. The synchronizer plans in real time the flight track of the flight accompanying unmanned plane according to the relative position relation, generates a flight construction controlling the flight accompanying unmanned plane, controls the flight of the flight accompanying unmanned plane, and ensures that the relative position relation is within a preset range. The aerial photographing equipment automatically tracks and photographs the main flight aircraft. The a flight accompanying unmanned plane carrying the aerial photographing equipment is utilized to photograph the main flight aircraft that is flying, and a position identification and synchronization mechanism is also adopted, so a photographing process is effectively completed.
Owner:高域(北京)智能科技研究院有限公司

Aspect-level sentiment analysis method based on dependency syntax tree and deep learning

The invention provides an aspect-level sentiment analysis method based on a dependency syntax tree and deep learning. The method comprises the steps of performing word segmentation and embedding training processing on a to-be-analyzed text to obtain word vector expression of each word in the text, and inputting the word vector expression into a bidirectional long-short-term neural network to obtain integrated information of each word and the text; constructing a dependency syntax tree by using all words in the text, constructing a GCN graph by using the dependency syntax tree, and performing iterative processing on the integrated information of the text and the GCN graph to obtain dependency syntax tree representation of an evaluation object in the text; and combining the integrated information of the text with the dependency syntax tree representation of the evaluation object, and performing analysis processing on a combined result by using a CNN to obtain an emotion prediction resultof the text for the evaluation object. According to the method, the semantic information of the text is effectively utilized, meanwhile, the importance of the evaluation object in aspect-level sentiment analysis is emphasized, and the accuracy of aspect-level sentiment analysis tasks of known evaluation objects is improved.
Owner:BEIJING JIAOTONG UNIV

APF and TSF hybrid compensation device for electric rig

The invention discloses an active power filter (APF) and thyristor switched filter (TSF) hybrid compensation device for an electric rig, which comprises a passive part, an active part, an electric quantity data acquisition module of a well site and the compensation device, a control module of a TST, and a control module of an APF. The filtering characteristics of the TSF are improved by utilizing the APF, so that when the TSF works in a combined manner, 2 to 10 times of harmonic currents injected into a power supply system of the well site are controlled within a given value, and the harmonic currents of the well site are prevented from being amplified when different filtering branches of the TSF are switched in a combined manner; and by adopting the structure that the APF is connected in parallel with a fundamental resonance module of a fifth filtering branch of the TSF through a coupling transformer, the capacity of the APF is very small, so that the APF is beneficially controlled, the cost of the whole set of device is reduced, the problem of overlarge harmonic currents occurring when the TSF is switched in a combined manner is effectively solved, and then the tasks of reactive compensation and harmonic elimination of the well site can be completed more safely and more effectively.
Owner:SHANDONG AITE MECHANICAL & ELECTRICAL TECH

Correction method of initial position in repeating motion of redundant mechanical arm

The invention discloses a correction method of an initial position in repeating motion of a redundant mechanical arm. The correction method comprises the following steps that 1) a desired target trajectory r*(t) and a desired retractable joint angle theta*(0) of an end effector of the redundant mechanical arm are determined, a final state attraction and optimization index is designed, and thus a mechanical arm repeating motion planning scheme is formed, wherein an initial joint angle during actual motion of the redundant mechanical arm can be designated freely and the end effector is not required to be located on a desired trajectory; 2) the initial joint angle theta (0) during the actual motion of the redundant mechanical arm is given, and by taking theta (0) as a motion starting point, anovel repeating motion planning scheme is converted to a corresponding quadratic programming problem; 3) a final state neural net model of a limited value activation function is constructed and a matrix equation is changed during solution of a limited value final state neural net; and 4) a solved result is used for controlling various joint motors and driving the mechanical arm to perform a task.The correction method of the initial position in the repeating motion of the redundant mechanical arm has the advantages of high precision and finite time convergence.
Owner:ZHEJIANG UNIVERSITY OF SCIENCE AND TECHNOLOGY

Attitude-orbit integrated control oriented multi-execution mechanism cooperative control distribution method

The invention discloses an attitude-orbit integrated control oriented multi-execution mechanism cooperative control distribution method and relates to a multi-execution mechanism cooperative control distribution method. The invention is aimed at solving the problems of low utilization rate of thruster fuel and little mutual cooperation among execution mechanisms of existing attitude-orbit integrated control oriented distribution strategy. In the invention, the orbit control expectation control force and the attitude control expectation control torque are distributed among the thrusters enabling both orbit control and attitude control; in the distribution process, the needs of track control are met first, and a thruster control distribution scheme proximal to the attitude control expectation control moment is optimally solved without additionally consuming redundant fuel; and after that, the remaining expectation control moment only can be distributed among the attitude-control execution mechanisms. While the attitude-orbit integrated control task is finished, the fuel consumption of the thruster is reduced, the burden on the attitude-control execution mechanisms such as flywheels and magnetic moments is alleviated, and the in-orbit life of spacecraft is prolonged. The method disclosed by the invention is applied to the field of spacecraft control.
Owner:HARBIN INST OF TECH

Formation control method for fusing global information and local information

The invention discloses a formation control method for fusing global information and local information. The method comprises the following steps: in an aircraft formation control process, firstly, planning a flight path of a lead aircraft in a ground control system, and determining flight parameters such as a desired flight path and a desired speed of the lead aircraft; in an actual flight process, calculating a flight path guide point of the lead aircraft according to a real-time state of a global desired flight path of the lead aircraft, and calculating a flight path guide point of a wing aircraft according to formation parameters; under a local coordinate system of the lead aircraft, calculating a local formation error between the lead aircraft and the wing aircraft in real time; in anaircraft control process, calculating a main control instruction according to the flight path guide point, calculating a secondary correction instruction according to the local formation error, and adding up the two instructions to obtain an actual control instruction of the aircraft, and controlling formation flight. On the basis of guaranteeing formation and realizing global flight path tracking, the formation control method can effectively improve the rapid convergence of formation control, the accuracy of the control process and the safety of tight formation flight, so as to effectively complete a formation flight mission.
Owner:NAT UNIV OF DEFENSE TECH

Dredged and concealed waterproof (and heat-insulating) system

The invention discloses a dredged and concealed waterproof (and heat-insulating) system which is characterized in that waterproof/heat-insulating plates which respectively take a smooth (or appropriate-gradient) temporary low (or high) curved surface or inclined surface of which the bottom is provided with an arc, inverted-U shaped or inverted-V shaped part and the like as a flow diversion structure are mutually connected, and joints or upper surfaces of the waterproof/heat-insulating plates are filled or sealed with waterproof mortar or other appropriate materials, so that rain water directly flows to a drainage system mainly from the upper surface of the system; after the flow diversion structure diverts the rain water leaked from joints or gaps of the waterproof/heat-insulating plates to the lowest part of the diverting curved surface or inclined surface, the rail water drips or flows into a preset drainage structure and then is intensively drained; and through carrying out appropriate concealing and adding a heat-insulating layer on the flow diversion structure and a drainage ditch, the system is better in appearance and wider in applications and can complete waterproofing and heat-insulating tasks. The system does not have high requirements for construction sites, processes and weathers, and has a long waterproof duration; and meanwhile, the system can be subjected to standardized prefabricated component production and also can be subjected to in-situ casting by using moulds, thereby reducing the construction difficulty and the production cost.
Owner:龙宏元

Emergency obstacle avoidance automatic-driving assistance torque calculation method based on intention of driver

The invention discloses an emergency obstacle avoidance automatic-driving assistance torque calculation method based on intention of a driver. The emergency obstacle avoidance automatic-driving assistance torque calculation method based on intention of the driver comprises the steps that first, the behavior of the driver is used as the input to identify the current intention of the driver, a Mobiey sensor is used for collecting information required for vehicle emergency obstacle avoidance path planning in real time, a chaotically optimized artificial potential field emergency obstacle avoidance automatic-driving assistance control method is used for solving optimal steering assistance guiding torque, people are assisted to drive a vehicle, and the driving state of the vehicle is changed; and then the input of the driver and vehicle state parameters after an emergency obstacle avoidance assistance system is involved are used as the input to identify the intention of the driver at the moment for the second time; and finally, based on the judgment result of the two-time intention of the driver, it is determined whether a steering assistance guidance torque complete involving method isadopted to complete the emergency obstacle avoidance working condition of the vehicle or not. The intention of different drivers can be effectively identified, amount of calculation is small, real-time control is achieved conveniently, the planned obstacle avoidance assistance steering torque is safer and more reliable than a traditional method, and the emergency obstacle avoidance working condition can be effectively completed.
Owner:LIAOCHENG UNIV

Test device for service life of aircraft alternating current generator fuel oil and slide oil radiator

The invention discloses a test device for the service life of an aircraft alternating current generator fuel oil and slide oil radiator. The test device for the service life of the aircraft alternating current generator fuel oil and slide oil radiator comprises a slide oil side normal temperature system, a slide oil side high temperature system, a fuel oil side normal temperature system, a fuel oil side high temperature system, a refrigeration system, an automatic control system and an environment cabin. According to the technical scheme, a plurality of fuel oil and slide oil radiator bodies can be subjected to cyclic fatigue tests of flow rate, pressure, temperature and ambient temperature; under the test system, high-temperature, high-pressure and large-flow slide oil is introduced intoa product; after test conditions are stable, the automatic control system is used for automatically switching, and low-temperature, low-pressure and small-flow slide oil is introduced into the product, therefore, the impact of oil flow rate, pressure and temperature can be verified to simulate the influence of oil flow rate, pressure, temperature and environment temperature of an aircraft on the service life of the product. The test flow rate, pressure and temperature are automatically detected, adjusted, collected and recorded by the automatic control system for each detection point on a pipeline, and feedback control and data recording are carried out through the collection parameters of each detection point.
Owner:GUIZHOU YONGHONG AVIATION MACHINERY

Unmanned aerial vehicle trajectory tracking method based on differential flatness characteristics

ActiveCN112241125AEasy to trackReduce the computational complexity of online optimizationAdaptive controlComputation complexityFlight vehicle
The invention discloses an unmanned aerial vehicle trajectory tracking method based on differential flatness characteristics, which comprises the following steps: performing dynamics and kinematics modeling on a four-rotor aircraft, performing differential flatness attribute judgment on a model of the four-rotor aircraft, and converting an underactuated four-rotor model into a full-drive system through nonlinear change on the basis of the property. And setting a virtual control quantity, decoupling the highly coupled system, and converting the highly coupled system into a linear system. The flight path tracking control problem of a constrained system is processed through model prediction control, a polyhedron description system is constructed for the time-varying characteristics of the system and comprises an original time-varying system, the online optimization calculation complexity is reduced, and a real-time terminal penalty value enabling the system to be stable is deduced according to the online optimization calculation complexity. The model prediction control method for the time-varying system is designed, constraints and system time-varying characteristics in the unmanned aerial vehicle trajectory tracking process are processed, the unmanned aerial vehicle trajectory tracking task can be effectively completed, the nonlinear characteristics of the unmanned aerial vehicleare well processed, the calculation complexity is low, and the tracking speed is high.
Owner:BEIJING INSTITUTE OF TECHNOLOGYGY

Detachable setup package applied to aluminum alloy template pre-buried part and method

The invention discloses a detachable setup package applied to an aluminum alloy template pre-buried part and a method. The detachable setup package comprises an aluminum alloy template, a pre-buried hole part and a rod part. One end of the pre-buried hole part abuts against the aluminum alloy template. One end of the rod part is detachably connected with the aluminum alloy template, and the otherend of the rod part penetrates through the pre-buried hole part. A cover plate is arranged on the other end face of the pre-buried hole part, raised back ribs abutting against the inner wall face of the pre-buried hole part and symmetrically arranged are arranged on the abutting face of the cover plate and the pre-buried hole part, the rod part is connected with a pin sheet arranged on the end face of the cover plate after sequentially penetrating through the pre-buried hole part and the cover plate, and a pin hole corresponding to the pin sheet is formed in the rod part. The detachable setuppackage can safely, rapidly and effectively complete fixing construction of the pre-buried hole part in a water supply and drainage discipline, and solves the problems that fixing of an existing rivetis difficult in construction, and leakage is prone to being generated, the mounting quality of a pre-buried part is ensured, and the purpose that fixing and mounting work of the pre-buried part in aconstruction site is completed safety, rapidly and effectively is achieved.
Owner:CHINA RAILWAY NO 5 ENG GRP BUILDING ENG
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