The sensing system of body movement is the key to realize compliant control and human-robot coupling for the exoskeleton robot. The dynamic model of the lower limb was analyzed and the cooperative control method was brought forward. Position control method was applied in the support phase, and the interactive-force based admittance control method was applied in the swing phase. According to the method, the sensing system of lower limb exoskeleton robot based on multi-information fusion was developed, which employed joints angle of body, human-machine interaction force and plantar pressure as perceptual parameters. Using the variable-gain Kalman fliter algorithm to process the angle measured by IMU sensor and the Savitzky-Golay filter algorithm to process the pressure measured by FSR, the gait characteristic was acquired and the test was carried out to verify the reliability of the method. The experimental results showed that the attitude angle calculating algorithm of IMU data had the characteristics of high precision and good stability, and the human-robot interactive method and the FSR pressure data processing algorithm were feasible, which meant that the sensing system had the reliable ability to acquire and fuse attitude angle, interaction force and plantar pressure and identify the wearer's gait accurately. The results can provide a reference for optimizing the sensing system of exoskeleton robot and promote the development of the control systems and strategies of exoskeleton robot.
When the field test of rope pulled automatic catwalk was carried out, the load fluctuation of rope was obvious, and it was difficult to complete the lifting of the target weight column. Therefore, the structure and motion characteristics of rope pulled automatic catwalk were analyzed, and dynamic model based on the D'Alemebert principle was established, MATLAB software was used to analyze the influence of the distance between the block on the base and the bottom of the ramp, the hinge position of the transfer arm and the support arm, and the length of the support arm on the load of rope. The analysis results showed that adjusting the position of block on the base to the bottom of the ramp, and reducing the length of support arm could reduce the required force of rope in the process of lifting. According to the analysis results, the structure size of automatic catwalk was adjusted to carry out the field test, the test result showed that the maximum lifting oil pressure of the hydraulic which was decreased by more than 2 MPa, the lifting capacity of automatic catwalk was improved. The analysis and experimental results can guide the design and optimization of rope pulled automatic catwalk.
Aiming at the design of cultural product modeling,design elements related to product modeling were subdivided into five aspects, including function, behavior, culture, emotion and structure method. Cultural and creative product concept prototype system was built to design culture creative products by combining case-based design technology, genetic algorithm and shape grammar knowledge. The system was built to guide designers to design some cultural products. A multi-objective optimization model of design element oriented on product modeling was proposed, and the matching operations on the user demand was made. The design method model of cultural products modeling was presented, which combined with the knowledge of product gene tree crossover operation and shape grammar, and a crossing and recombinant of design elements between modern products and cultural artifacts was made. Through the in-depth study of product modeling design elements, and integrating case-based reasoning, genetic algorithm and the shape grammar knowledge into cultural and creative product concept prototype system, it was proved that the system was able to aid the designers to make some creative designs. An example of the design on small speakers was used to verify the feasibility of this method. An effective design method on cultural product design is provided.
In order to ensure the safety of antenna system at launch moment and orbit stage, the vibration property of a data transmission antenna developed to work on lunar orbit satellite was analysed. Through the finite element modeling and simulation method,the vibration performance of the antenna on high orbit satellite at launch moment and orbit stage was analysed and calculated, and the system antenna structure was optimized according to the simulation results. The vibration test for antenna system was applied in actual vibration environment, and the results indicated that the antenna system structure was reliable. The electrical property was tested again after vibration test, and the result indicated that the antenna electrical property was stable. The result of vibration test confirmed the reliability of the antenna and the credibility of the finite element analysis. This antenna has been launched and worked on orbit with stable performance indexes and good work conditions. This study can prefer some reference to increase the vibration safety for the related satellite antenna.
Aiming at the problems existing in the automatic feeding, quantitative filling process of the capacitor aluminum shell such as low automation degree, low filling accuracy and so on, the control system of automatic feeding and quantitative filling for the capacitor aluminum shell was designed. The PLC of Mitsubishi FX3GA series was used to conduct the reasonable configuration of hardware and software for the control system and the hardware composition and software flow of the system were designed in detail. The touch screen of Mitsubishi GS series was used to achieve the system parameter modification and state monitoring. The system had been applied in the practical application of capacitor production enterprise and application effect showed that the system ran reliably and stably, the operation period was 10 s, the error of the quantitative filling for aluminum shell was less than 2%, and the product quality and production efficiency were improved, which could meet the production requirements of enterprises. The system has a certain popularization value.
In order to eliminate the redundant moment of force of the electric load simulation system (ELSS) and improve the output accuracy of the system loading torque, a kind of adaptive control method for eliminating position disturbance torque of steering engine was designed. Based on the feed forward control and adaptive control theory, the effectiveness of the method was analyzed by MATLAB simulation software and the experimental verification was carried out. Simulations and experimental results showed that the method could adaptively adjust the system loading error, and the higher the frequency of the steering engine was, the longer the tracking error could be adjusted. In the same conditions of the loading torque and amplitude phase of the steering engine, the higher the steering engine frequency was, the more obvious the inhibitory effect of the control method to the redundant moment of force was. In the same conditions of the loading torque and movement frequency of the steering engine, the greater the amplitude phase of steering engine was, the more obvious the inhibitory effect was. The method can stabilize the system in an ideal output state by the output of the reference model when the actual system parameters are unknown or gradually changing. The research results have certain reference values for the design of aircraft electric load simulator.
Aiming at the problems such as the low design efficiency of aviation blade die, serious wear and difficulty in parameters correction, based on UG/Open API, the die CAD system was developed by analysis of the blade die design process, and the parametric design of die was realized and die design efficiency was improved. Based on Archard correction theory, the influence of die design parameters on the precision forging of the blade was simulated by Deform-3D software. The influence of forging speed, the forming angle and the thickness of the bridge on the wear and life of the blade were analyzed by orthogonal test. The optimal combination parameters beneficial to extend the die life were determined and the design rules of them were optimized. It was accurate and simple to make the die design parameters be determined. Through the engineering experiment, the die wear and life were analyzed and the results were in good agreement with the simulation results. It is of great significance to optimize the design and wear analysis of air forging die.
In order to improve the sealing reliability of the lead wire from the pressure chamber in the high pressure environment and ensure that the electronic equipment used in the downhole tool can work under atmospheric pressure, a kind of injection class high pressure sealing connector was designed. The sealing connector which filled with rubber and epoxy resin was analyzed based on the finite element software, and the experimental verification was carried out. Analysis and experiment results showed that when the filling material was rubber, the sealing property was good, but the material was easy to be squeezed out, and 88°was a better choice for the semi-cone angle of shell body. When the filling material was epoxy resin, material protrusion could be avoided, but there would be liquid leaking in a certain pressure range. When the filling material was rubber and epoxy resin, evagination distance decreased with increasing of epoxy resin and the use ratio of epoxy resin 40% was a good choice. High pressure sealing connector mainly relied on first five threads to bear load. The maximum stresses appeared at the minor diameter between first thread and second thread of shell body. The maximum stresses of contact pin appeared at the upper border between rubber and epoxy resin. The researching achievement has certain significance for design of high pressure sealing connector and selection of filling material.
To study the mechanical property of guide foot, the detecting system, which was based on non-destructive testing technology (NDT Tech), in which the pin sensors was installed with the same strength as the core shaft of guide foots and whose signal was transmitted online by wireless signal launcher, was designed to detect the force of guide foot under different conditions online by analyzing the force of the pin. Then the field test showed that, under the condition of oblique cutting, the loads of guide foots were at random, and the effective values of ear-plates' loads were 26.1 kN and 15.1 kN in the left guide foot and the right are 45.1 kN and 21.5 kN. By FEA, it's known that the places, where were the maximum stress of the left guide foot and the right one, which were 173.87 MPa and 187.85 MPa, were located at ear-plate of guide foot in the circumstances of maximal force. And testing and analysis results provide substantial theoretical and numerical basis for the design optimization of guide foots.
Aiming at the requirements of real-time interaction between the gait rehabilitation training robot and the patient,a sensing system for the contact force between them was developed. The lower limb exoskeleton robot dynamics model including the active force of human was established by Lagrange method,and the patient's lower limb movement intentions were analyzed to provide judgment criterions for the interactive control in gait rehabilitation training. The static and dynamic measurement experiments and the passive/active rehabilitation training measurement experiments were carried out on the gait rehabilitation training robot prototype system. The results showed that the sensing system could satisfy the detecting accuracy requirements for human-robot contact force, and acquire human movement intention in the rehabilitation training. The design of the human-robot interactive information sensing system lays a foundation for the research on the intelligent interactive control strategy of gait rehabilitation training robot.