5 results about "Interconnectivity" patented technology

A rack may include a frame having vertical uprights and transverse members coupled together so as to form boundaries of an internal volume of the rack. The boundaries may include a first lateral face, a second lateral face, a front face, and a back face. A cartridge can be installed forward or rearward of the front face and laterally inward from the first lateral face or the second lateral face. Cables may be connected between the cartridge and a plurality of appliances. The cables may include a first cable extending between the cartridge and a first appliance supported by the rack. The cables may further include a second cable extending between a second appliance and the cartridge so as to establish a signal path between the first appliance and the second appliance through the first cable, the cartridge, and the second cable.

SYSTEM AND METHOD FOR PROVIDING INTERCONNECTIVITY BETWEEN COMPONENTS OF A MANO FRAMEWORK The present disclosure relates to system (108) and method (700) for providing interconnectivity between components of MANO framework The method (700) includes receiving (702), by a network function virtualization orchestrator (NFVO) (304), at least one service request from an event routing manager (ERM) (208, 302) via an associated network interface. The method (700) includes extracting (704), by the NFVO (304), one or more parameters from the at least one received service request. The method (700) includes processing (706), by the NFVO (304), the at least one received service request based on the extracted one or more parameters to generate at least one orchestration request. The method (700) includes determining (708), by the NFVO (304), at least one network service associated with at least one component of the MANO framework based on the at least one generated orchestration request. Ref.

1. The name of the design product: home interconnection coaxial device. 2. The use of the design product: realize the data communication in the home through the coaxial cable. 3. The design points of the design product: in shape. 4. The picture or photo that can best show the design points: perspective view.

The present invention discloses a method and device for analyzing inter-well connectivity based on LAE. For the historical injection and production data of an oilfield well group, LSTM-AE is used to encode the water injection volume sequence, construct a vector representation of the water injection volume sequence, and input this vector into a fully connected layer to predict the liquid production volume of production wells. The water injection volumes of each water well in the well group are used as input variables for sensitivity analysis, and the global sensitivity analysis method EFAST is applied to analyze the sensitivity of the input variables of the liquid production volume prediction model based on LSTM-AE. By decomposing the variance of the model prediction results, the influence of the water injection volumes of each water well and the coupling effect between the water injection volumes of water wells on the model results is obtained to calculate the parameter sensitivity index, identify the key water injection wells that have a significant impact on the liquid production volume of production wells, and clarify the inter-well connectivity status. The present invention can accurately and effectively analyze the inter-well connectivity.

The invention discloses a spacecraft formation tracking control method, device, equipment and medium, relates to the technical field of spacecraft control, is applied to a controller in a target spacecraft formation, and comprises the steps: determining each topological neighbor set according to the interaction connectivity of each spacecraft in the target spacecraft formation, inputting a potential collision set in the topological neighbor set into a preset formula constructed based on an artificial potential function, and inputting the output collision avoidance control information into a preset formula constructed based on controller design parameters to obtain an initial formation tracking control signal; the design parameters are designed based on an immersion and invariant algorithm and a preset performance function; processing the initial formation tracking control signal based on an event triggering mechanism so as to obtain a control error input signal by using the obtained final formation tracking control signal; and when the control error input signal meets a preset triggering condition, the collision avoidance control information is transmitted to an actuator of each spacecraft, and tracking control is realized. And accurate tracking and low-cost control are carried out on the spacecraft formation.