15 results about "Remote guidance" patented technology

The invention relates to the field of electric power systems, in particular to an electric power facility remote intelligent maintenance method and system. The method comprises the following steps: collecting three kinds of heterogeneous monitoring data of vibration spectrum, infrared thermal imaging and partial discharge signals; mapping the data to a three-dimensional feature fusion space, and calculating a mahalanobis distance to generate a fusion feature matrix; extracting spatio-temporal features by using a convolutional long-short-term memory network, and outputting a triple diagnosis result including a fault type, a severity level and an evolution trend; searching a dynamic maintenance scheme in a maintenance strategy knowledge graph based on the diagnosis result; solving an optimal resource scheduling scheme by adopting an improved Hungary algorithm in combination with the geographic topology and the resource state; the maintenance operation is remotely guided through the augmented reality terminal, and real-time verification is carried out; and collecting the maintained data, carrying out residual analysis, and reversely optimizing the knowledge graph. The method realizes full-process intelligent management, improves timeliness and reliability of operation and maintenance of electric power facilities, and is suitable for a remote intelligent maintenance scene of an electric power system.

The application relates to the technical field of medical equipment, and particularly discloses a head-mounted operation camera system and method, wherein the system comprises a shell; a main control board is arranged in the shell; a universal joint is connected to the front of the shell; and a camera module is connected to the universal joint; the camera module comprises a front cover and a rear cover; a CMOS module is arranged between the front cover and the rear cover; a replaceable optical filter is arranged in front of the front cover; and the replaceable optical filter and the front cover are both provided with magnets; an image processing module arranged in the main control board sequentially completes original image processing, exposure regulation and control, stroboscopic suppression, focus calibration, resolution optimization and color correction to generate optimized image data. The main control board analyzes the image in real time, evaluates the image quality, drives the CMOS module to optimize the acquisition parameters and continues to acquire, and forms a closed-loop imaging regulation and control mechanism; the real-time remote guidance and postoperative review improve the operation quality. The rear of the shell and the front of a separate wearing and fixing sheet are provided with multiple-stage magnet sheets, the shell is fixed on the head of an operator through clamping of an operating cap, and the shell is convenient to wear and deploy.

The invention is suitable for the technical field of medical imaging, and provides a robot remote guidance method, device and system, and the method comprises the steps: obtaining a left and right eye image group sequence collected by a binocular camera through first electronic equipment of an operation end, and determining a target disparity map of each left and right eye image group, taking the integer part and the decimal part of the pixel value of each pixel in the target disparity map as a first channel value and a second channel value respectively, taking a preset placeholder as a third pixel value of the pixel to obtain a three-channel disparity map, and compressing the three-channel disparity map and the reference image into a target compressed file, sending the target compressed file and the parameter information of the binocular camera to the head-mounted device of the guidance end; and the head-mounted device restores the target three-dimensional coordinates and the color information of each spatial point from the target compressed file according to the parameter information, and renders and displays all spatial points according to the target three-dimensional coordinates and the color information, so that the data transmission efficiency and the data quality can be improved on the premise of ensuring the accuracy of remote operation guidance.

The application is a kind of method for remotely guiding infrared observation equipment to observe target, belonging to the technical field of remote guidance, which comprises the following steps: a remote control terminal locates the observation target and obtains target position information, and then wirelessly transmits the target information to first, second and third infrared observation equipment; the remote control terminal estimates the optimal observation distance based on the estimated size of the target and the field of view angle and resolution of the first infrared observation equipment; the remote control terminal guides the first, second and third infrared observation equipment to move to the optimal observation distance from the target position and to the positions of the three apexes of the inscribed regular hexagon in the circle for cooperative target observation; the remote control terminal remotely controls the real-time adjustment of the direction, position and focal length of each infrared observation equipment based on the video stream images returned by the first, second and third infrared observation equipment. The application is used to remotely and real-timely guide infrared observation equipment to observe the specified target.

Disclosed are a remote medical guidance method and system based on virtual reality, belonging to the technical field of medical guidance. The method includes: obtaining an action sequence of remote guidance personnel for medical operations; and generating a three-dimensional operation model based on the action sequence and displaying the three-dimensional operation model in an operation live scene. The present disclosure achieves remote guidance of medical operations based on virtual reality, eliminating the need to relocate patients or medical personnel and avoiding missing the optimal treatment time window.

The invention discloses an infant airway collaborative intubation safety control system based on different-place mixed reality. The system aims at solving the problems of space synchronization robustness and predictive time delay compensation in remote guidance, a mapping relation between a local coordinate system and a remote coordinate system is established through a space synchronization module, a long short-term memory (LSTM) network is used for predictive compensation of a remote expert track, and visual lag is eliminated. The core safety mechanism comprises the steps that the airway dynamic model module generates a real-time dynamic signed distance field (D-SDF); the risk prediction module calculates the dynamic collision risk probability of the laryngoscope tail end and the dynamic airway wall in real time. The tactile feedback device responds to the risk probability, adopts a variable admittance control strategy, generates an operation viscous sense by nonlinearly increasing virtual damping, and activates a virtual stiffness item pointing to a safety area when the risk exceeds a critical value, so as to apply a reverse elastic restoring force and realize active safety avoidance in a physical level. And the submillimeter precision and safety of the airway operation of the infant are ensured.

The present invention discloses a rapid iterative guidance method for lunar orbit rendezvous and remote guidance, comprising: obtaining an initial orbital state corresponding to an initial moment and an orbital target state corresponding to a terminal moment; establishing a nonlinear equation group of design variables and terminal orbital states; transforming the nonlinear equation group of design variables and terminal orbital states based on the near-circular orbit element representation of the terminal orbital state and the orbital target state; determining iterative initial values ​​and convergence conditions; iteratively solving the nonlinear equation group of the transformed design variables and terminal orbital states based on the determined iterative initial values ​​and convergence conditions until the convergence conditions are met, obtaining the final design variables, and completing the guidance. The method of the present invention has high iterative efficiency and fast calculation speed, is applicable to any number of orbit changes, and the components of each orbit change can be arbitrarily specified. It is particularly applicable to the needs of on-orbit real-time generation of lunar orbit rendezvous and remote guidance orbit change strategies and reconstruction of remote guidance strategies under fault conditions.

A system for guiding a drone to an intended destination using a remote guidance system, independent of a global positioning system installed on the drone and independent of radio guidance. The system uses a two-way optical communication channel between the guidance system and the drone. The drone and the guidance system each have a light source emitting a beam of encoded light, such as a modulated laser beam, and having an extended field of illumination, and a detector receiving the impinging light beam. The guidance system can detect the angular location of the drone emission, and can transmit instructions optically to the drone, while the drone can receive flight path instructions from the guidance system. The drone can be launched from a position that is not in the line of sight of its intended destination and guided optically from the launch position to its intended target destination.

1. The name of the design product: sleep monitor (multiple lead). 2. The use of the design product: for people with symptoms of sleep breathing disorders (suspected) to complete wearing at home combined with remote guidance, and to monitor physiological parameters during sleep, to realize portable sleep breathing disorder screening and provide medical basis for subsequent diagnosis and treatment. 3. The design points of the design product: in shape. 4. The picture or photo that best indicates the design points: combined state reference drawing.

According to the remote monitoring system and method for the in-vitro liver perfusion equipment, medical staff can move and operate a tablet personal computer within a certain range in an operating room without constraint of the physical position of an equipment host, a patient and the equipment can be taken into consideration at the same time, it can be guaranteed that the equipment is normally controlled in a small space or in a multi-person operation scene, and the operation efficiency is improved. The flexibility of the working process is improved; through the Internet cloud, remote specialists can observe the whole perfusion process in real time as if they are personally on site, so that instant remote guidance is provided for evaluation of marginal donor liver and processing of complex conditions, and the utilization efficiency and the treatment level of medical resources are improved; the dual network architecture provides communication redundancy to a certain extent. Based on the alarm pushing function of the cloud platform, 7 * 24-hour state monitoring is realized, even if field personnel leave temporarily, key alarms can be known in time through mobile phones, and the safety is greatly improved.

The invention provides a long-distance guidance real-time deviation prediction method based on a pulse guidance model. The long-distance guidance real-time deviation prediction method based on the pulse guidance model comprises the steps that 1, the instantaneous orbit number of a tracker and the instantaneous orbit number of a target device at the t0 moment are obtained; 2) obtaining an autonomous rendezvous and docking guidance sequence which is autonomously planned by the tracker and is not executed; (3) tf is taken as a predicted time end point, and if it is judged that the equivalent starting time of the ith guidance pulse is within the range of [t0-tf], the step (4) is executed; otherwise, turning to step 8); 4) calculating to obtain an orbit instantaneous root before ith orbit control; 5) calculating a tracker instantaneous orbital element variable quantity caused by guidance control; 6) calculating the instantaneous orbital element of the tracker after guidance pulse control; 7) guiding pulse times i + 1; if i is less than or equal to n, turning to the step 4); otherwise, turning to step 8); 8) calculating a free flight orbit set; 9) calculating a relative trajectory under the target orbital system; and 10) calculating to obtain the deviation of the long-distance guide terminal.

The application is suitable for the field of medical imaging technology, and provides a robot remote guidance method, device and system. The method comprises the following steps: a first electronic device of an operation end acquires a left-eye image group sequence and a right-eye image group sequence collected by a binocular camera, determines a target disparity map of each left-eye image group and right-eye image group, takes an integer part and a decimal part of a pixel value of each pixel in the target disparity map as a first channel value and a second channel value respectively, takes a preset placeholder as a third pixel value of the pixel, obtains a three-channel disparity map, and compresses the three-channel disparity map and a reference image into a target compressed file, so as to send the target compressed file and parameter information of the binocular camera to a head-mounted device of a guidance end; the head-mounted device restores target three-dimensional coordinates and color information of each spatial point from the target compressed file according to the parameter information, and renders and displays all spatial points according to the target three-dimensional coordinates and the color information, so that the data transmission efficiency and data quality are improved under the premise of ensuring the accuracy of remote surgery guidance.

The application provides a terminal window adjustment method for super-fast rendezvous and docking remote guidance, and relates to the technical field of rendezvous and docking. The method comprises the following steps: acquiring guidance parameters of two-pulse guidance used by a tracking spacecraft in a remote guidance section; wherein the guidance parameters comprise a first pulse, a second pulse and a preset execution time of the second pulse; after the first pulse ends, predicting a first position of the tracking spacecraft at the terminal of the remote guidance according to the second pulse and the preset execution time; when the first position is not in a trace direction position fluctuation range of the terminal of the remote guidance, adjusting the preset execution time to complete the adjustment of the terminal window. The terminal window adjustment method for fast rendezvous and docking remote guidance can adjust the terminal window of the remote guidance, improve the accuracy of the terminal of the remote guidance and complete the super-fast rendezvous and docking task.