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Power Consumption Characteristics Research on Mobile System of Electrically Driven Large-Load-Ratio Six-Legged Robot

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Chinese Journal of Mechanical Engineering 2023年第1期36卷 237-267页

作者： Hongchao Zhuang Ning Wang Haibo Gao zongquan deng School of Mechanical Engineering Tianjin University of Technology and EducationTianjin300222China School of Information Technology Engineering Tianjin University of Technology and EducationTianjin300222China State Key Laboratory of Robotics and System Harbin Institute of TechnologyHarbin150001China

The electrically driven large-load-ratio six-legged robot with engineering capability can be widely used in outdoor and planetary ***,due to the particularity of its parallel structure,the effective utilization rate of energy is not high,which has become an important obstacle to its practical *** research the power consumption characteristics of robot mobile system is beneficial to speed up it toward *** on the configuration and walking modes of robot,the mathematical model of the power consumption of mobile system is set *** view of the tripod gait is often selected for the six-legged robots,the simplified power consumption model of mobile system under the tripod gait is established by means of reducing the dimension of the robot’s statically indeterminate problem and constructing the equal force ***,the power consumption of robot mobile system is solved under different working *** variable tendencies of the power consumption of robot mobile system are respectively obtained with changes in the rotational angles of hip joint and knee joint,body height,and *** articulated rotational zones and the ranges of body height and span are determined under the lowest power *** to the walking experiments of prototype,the variable tendencies of the average power consumption of robot mobile system are respectively acquired with changes in duty ratio,body height,and ***,the feasibility and correctness of theory analysis are verified in the power consumption of robot mobile *** proposed analysis method in this paper can provide a reference on the lower power research of the large-load-ratio multi-legged robots.

关键词： Electrically driven Large-load-ratio six-legged robot Power consumption Mobile system

Calibration of Discrete Element Heat Transfer Parameters by Central Composite Design

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Chinese Journal of Mechanical Engineering 2017年第2期30卷 419-427页

作者： zongquan deng Jinsheng CUI Xuyan HOU Shengyuan JIANG Department of Mechatronics Engineering Harbin Institute ofTechnologyHarbin 150006China

The efficiency and precision of parameter calibration in discrete element method （DEM） are not satisfactory, and parameter calibration for granular heat transfer is rarely involved. Accordingly, parameter calibration for granular heat transfer with the DEM is studied. The heat transfer in granular assemblies is simulated with DEM, and the effective thermal conductivity （ETC） of these granular assemblies is measured with the transient method in simulations. The measurement testbed is designed to test the ETC of the granular assemblies under normal pressure and a vacuum based on the steady method. Central composite design （CCD） is used to simulate the impact of the DEM parameters on the ETC of granular assemblies, and the heat transfer parameters are calibrated and compared with experimental data. The results show that, within the scope of the considered parameters, the ETC of the granular assemblies increases with an increasing particle thermal conductivity and decreases with an increasing particle shear modulus and particle diameter. The particle thermal conductivity has the greatest impact on the ETC of granular assemblies followed by the particle shear modulus and then the particle diameter. The calibration results show good agreement with the experimental results. The error is less than 4%, which is within a reasonable range for the scope of the CCD parameters. The proposed research provides high efficiency and high accuracy parameter calibration for granular heat transfer in DEM.

关键词： Granular assembly · Parameter calibration · Effective thermal conductivity (ETC) · Discrete element method (DEM) · Central composite design (CCD) · Vacuum

Virtual Simulation System with Path-following Control for Lunar Rovers Moving on Rough Terrain

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Chinese Journal of Mechanical Engineering 2012年第1期25卷 38-46页

作者： GAO Haibo deng zongquan DING Liang WANG Mengyu State Key Laboratory of Robotics and Systems Harbin Institute of TechnologyHarbin 150001China School of Mechatronics Harbin Institute of TechnologyHarbin 150001China

Virtual simulation technology is of great importance for the teleoperation of lunar rovers during the exploration phase, as well as the design of locomotion systems, performance evaluation, and control strategy verification during the R&D phase. The currently used simulation methods for lunar rovers have several disadvantages such as poor fidelity for wheel-soil interaction mechanics, difficulty in simulating rough terrains, and high complexity making it difficult to realize mobility control in simulation systems. This paper presents an approach for the construction of a virtual simulation system that integrates the features of 3D modeling, wheel-soil interaction mechanics, dynamics analysis, mobility control, and visualization for lunar rovers. Wheel-soil interaction experiments are carried out to test the forces and moments acted on a lunar rover’s wheel by the soil with a vertical load of 80 N and slip ratios of 0, 0.03, 0.05, 0.1, 0.2, 0.3, 0.4, and 0.6. The experimental results are referenced in order to set the parameters’ values for the PAC2002 tire model of the ADAMS/Tire module. In addition, the rough lunar terrain is simulated with 3DS Max software after analyzing its characteristics, and a data-transfer program is developed with Matlab to simulate the 3D reappearance of a lunar environment in ADAMS. The 3D model of a lunar rover is developed by using Pro/E software and is then imported into ADAMS. Finally, a virtual simulation system for lunar rovers is developed. A path-following control strategy based on slip compensation for a six-wheeled lunar rover prototype is researched. The controller is implemented by using Matlab/Simulink to carry out joint simulations with ADAMS. The designed virtual lunar rover could follow the planned path on a rough terrain. This paper can also provide a reference scheme for virtual simulation and performance analysis of rovers moving on rough lunar terrains.

关键词： lunar rover comprehensive simulation system rough terrain wheel-soil interaction mechanics path-following control

Effects of Joint on Dynamics of Space Deployable Structure

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Chinese Journal of Mechanical Engineering 2013年第5期26卷 861-872页

作者： GUO Hongwei ZHANG Jing LIU Rongqiang deng zongquan School of Mechanical and Electrical Engineering Harbin Institute of Technology

Joints are necessary components in large space deployable truss structures which have significant effects on dynamic behavior of these joint dominated *** researches usually analyzed effects of one or fewer joint characters on dynamics of jointed *** of joint stiffness,damping,location,number,clearance and contact stiffness on dynamics of jointed structures are systematically *** beam model containing linear joints is developed based on finite element method,influence of joint on natural frequencies and mode shapes of the jointed system are *** results show that frequencies of jointed system decrease dramatically when peak mode shapes occur at joint locations,and there are cusp shapes present in mode *** frequencies increase with joint damping increasing,there are different joint damping to achieve maximum system damping for different joint *** nonlinear force-displacement is described by describing function method,one-DOF model containing nonlinear joints is established to analyze joints freeplay and hysteresis *** results show that nonlinear effects of freeplay and hysteresis make dynamic responses switch from one resonance frequency to another frequency when amplitude exceed demarcation *** contact stiffness determine degree of system nonlinearity,while exciting force level,clearance and slipping force affect amplitude of dynamic *** responses of joint dominated deployable truss structure under different sinusoidal exciting force levels are *** test results show obvious nonlinear behaviors contributed by joints,dynamic response shifts to lower frequency and higher amplitude as exciting force *** test results are further compared with analytical results,and joint nonlinearity tested is coincident with hysteresis *** method of joint effects on dynamic characteristics of jointed system is proposed,which ca

关键词： deployable structure joint dynamic mode shape experiment

Method for Analyzing Articulated Torques of Heavy-duty Six-legged Robot

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Chinese Journal of Mechanical Engineering 2013年第4期26卷 801-812页

作者： ZHUANG Hongchao GAO Haibo DING Liang LIU Zhen deng zongquan State Key Laboratory of Robotics and System Harbin Institute of Technology

The accuracy of an articulated torque analysis influences the comprehensive performances of heavy-duty multi-legged robots. Currently, the extremal estimation method and some complex methods are employed to calculate the articulated torques, which results in a large safety margin or a large number of calculations. To quickly obtain accurate articulated torques, an analysis method for the articulated torque is presented for an electrically driven heavy-duty six-legged robot. First, the rearmost leg that experiences the maximum normal contact force is confirmed when the robot transits a slope. Based on the ant-type and crab-type tripod gaits, the formulas of classical mechanics and MATLAB software are employed to theoretically analyze the relevant static torques of the joints. With the changes in the joint angles for the abductor joint, hip joint, and knee joint, variable tendency charts and extreme curves are obtained for the static articulated torques. Meanwhile, the maximum static articulated torques and the corresponding poses of the robot are also obtained. According to the poses of the robot under the maximum static articulated torques, ADAMS software is used to carry out a static simulation analysis. Based on the relevant simulation curves of the articulated torques, the maximum static articulated torques are acquired. A comparative analysis of the maximum static articulated torques shows that the theoretical calculation values are higher than the static simulation values, and the maximum error value is approximately 10%. The proposed method lays a foundation for quickly determining accurate articulated torques to develop heavy-duty six-legged robots.

关键词： heavy-duty six-legged robot articulated torque MATLAB static simulation analysis ADAMS

Optimizing the Qusai-static Folding and Deploying of Thin-Walled Tube Flexure Hinges with Double Slots

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Chinese Journal of Mechanical Engineering 2014年第2期27卷 279-286页

作者： YANG Hui deng zongquan LIU Rongqiang WANG Yan GUO Hongwei State Key Laboratory of Robotics and System Harbin Institute of Technology

The thin-walled tube flexure（TWTF） hinges have important potential application value in the deployment mechanisms of satellite and solar array, but the optimal design of the TWTF hinges haven＇t been completely solved, which restricts their applications. An optimal design method for the qusai-static folding and deploying of TWTF hinges with double slots is presented based on the response surface theory. Firstly, the full factorial method is employed to design of the experiments. Then, the finite element models of the TWTF hinges with double slots are constructed to simulate the qusai-static folding and deploying non-linear analysis. What＇s more, the mathematical model of the TWTF flexure hinge quasi-static folding and deploying properties are derived by the response surface method. Considering of small mass and high stability, the peak moment of quasi-static folding and deploying as well as the lightless are set as the objectives to get the optimal performances. The relative errors of the objectives between the optimal design results and the FE analysis results are less than 7%, which demonstrates the precision of the surrogate models. Lastly, the parameter study shows that both the slots length and the slots width both have significant effects to the peak moment of quasi-static folding and deploying of TWTF hinges with double slots. However, the maximum Mises stress of quasi-static folding is more sensitive to the slots length than the slots width. The proposed research can be applied to optimize other thin-walled flexure hinges under quasi-static folding and deploying, which is of great importance to design of flexure hinges with high stability and low stress.

关键词： design optimization quasi-static folding and deploying flexure hinges thin-walled tube response surface method,numerical simulation

Sagittal SLIP-anchored task space control for a monopode robot traversing irregular terrain

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Frontiers of Mechanical Engineering 2020年第2期15卷 193-208页

作者： Haitao YU Haibo GAO Liang DING zongquan deng State Key Laboratory of Robotics and Systems Harbin Institute of TechnologyHarbin 150001China

As a well-explored template that captures the essential dynamical behaviors of legged locomotion on sagittal plane,the spring-loaded inverted pendulum(SLIP)model has been extensively employed in both biomechanical study and robotics *** at fully leveraging the merits of the SLIP model to generate the adaptive trajectories of the center of mass(CoM)with maneuverability,this study presents a novel two-layered sagittal SLIP-anchored(SSA)task space control for a monopode robot to deal with terrain *** work begins with an analytical investigation of sagittal SLIP dynamics by deriving an approximate solution with satisfactory apex prediction accuracy,and a two-layered SSA task space controller is subsequently developed for the monopode *** higher layer employs an analytical approximate representation of the sagittal SLIP model to form a deadbeat controller,which generates an adaptive reference trajectory for the *** lower layer enforces the monopode robot to reproduce a generated CoM movement by using a task space controller to transfer the reference CoM commands into joint torques of the multi-degree of freedom monopode ***,an adaptive hopping behavior is exhibited by the robot when traversing irregular *** results have demonstrated the effectiveness of the proposed method.

关键词： legged robots spring-loaded inverted pendulum task space control apex return map deadbeat control irregular terrain negotiation

Configuration synthesis of planar folded and common overconstrained spatial rectangular pyramid deployable truss units

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Chinese Journal of Aeronautics 2019年第7期32卷 1772-1787页

作者： Hui YANG Hongwei GUO Yan WANG Rongqiang LIU zongquan deng College of Electrical Engineering and Automation Anhui UniversityHefei230601China State Key Laboratory Robotics and System Harbin Institute of TechnologyHarbin150001China China Electronics Technology Group Corporation No.38Research Hefei230088China

Compared with non-overconstrained deployable units, overconstrained deployable units are widely used in space missions for their higher stiffness characteristics. Besides the performance of a three-step topological structural analysis and design of the rectangular pyramid deployable truss unit(PDTU), conducting a structural synthesis of an overconstrained deployable unit requires the determination of the relative position and direction of each kinematic axis. The structural synthesis of an overconstrained deployable unit is investigated based on screw theory and its topological structure. The possible overconstrained cases of the rectangular PDTUs are analyzed, and corresponding screw expressions are obtained. Thus, the rectangular PDTUs, which can be folded into a plane, are synthesized systemically, and a series of overconstrained rectangular PDTUs is obtained. Furthermore, the feasibility of the folded and deployed motions under one degree of freedom for those deployable units is verified in dynamical simulation by using ADAMS 2010.

关键词： Assembly SAR antenna Common overconstraint Deployable truss structure Screw theory Structural synthesis

Drilling load modeling and validation based on the filling rate of auger flute in planetary sampling

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Chinese Journal of Aeronautics 2017年第1期30卷 434-446页

作者： Quan Qiquan Tang Junyue Yuan Fengpei Jiang Shengyuan deng zongquan State Key Laboratory of Robotics and System Harbin Institute of Technology

Some type of penetration into a subsurface is required in planetary sampling. Drilling and coring, due to its efficient penetrating and cuttings removal characteristics, has been widely applied in previous sampling missions. Given the complicated mechanical properties of a planetary regolith, suitable drilling parameters should be matched with different drilling formations ***, drilling faults caused by overloads could easily happen. Hence, it is necessary to establish a drilling load model, which is able to reveal the relationships among drilling loads, an auger＇s structural parameters, soil＇s mechanical properties, and relevant drilling parameters. A concept for the filling rate of auger flute（FRAF） is proposed to describe drilling conditions. If the FRAF index under one group of drilling parameters is less than 1, this means that the auger flute currently removes cuttings smoothly. Otherwise, the auger will be choked with compressed cuttings. In drilling operations, the drilling loads on the auger mainly come from the conveyance action, while the drilling loads on the drill bit primarily come from the cutting action. Experiments in one typical lunar regolith simulant indicate that the estimated drilling loads based on the FRAF coincide with the test results quite well. Based on this drilling load model, drilling parameters have been optimized.

关键词： Coring Drilling load Filling rate of auger fluteLunar regolith simulant Planetary drilling