针对船体密封舱、箱柜等狭窄空间普遍存在的机器人难以工作问题,提出了一种新型6-DOF(degrees of freedom)机器人。首先分析了该机器人的机械结构,基于D-H坐标理论建立了机器人D-H坐标表格以及机器人正、逆运动学方程,其次应用MATLAB对...针对船体密封舱、箱柜等狭窄空间普遍存在的机器人难以工作问题,提出了一种新型6-DOF(degrees of freedom)机器人。首先分析了该机器人的机械结构,基于D-H坐标理论建立了机器人D-H坐标表格以及机器人正、逆运动学方程,其次应用MATLAB对机器人的运动学进行了仿真,结果表明所得的机器人正、逆运动学方程完全正确;最后设计了虚拟样机,利用RobotStudio仿真分析了机器人箱体焊接的优点;为进一步验证设计的机器人运动性能,与通用6-DOF机器人做了对比分析。研究结果表明新型机器人运动的可行性,为设计适应箱柜等狭窄空间的工业机器人提供了理论依据。展开更多
Because of its characteristics of simple algorithm and hardware, optical flow-based motion estimation has become a hot research field, especially in GPS-denied environment. Optical flow could be used to obtain the air...Because of its characteristics of simple algorithm and hardware, optical flow-based motion estimation has become a hot research field, especially in GPS-denied environment. Optical flow could be used to obtain the aircraft motion information, but the six-(degree of freedom)(6-DOF) motion still couldn't be accurately estimated by existing methods. The purpose of this work is to provide a motion estimation method based on optical flow from forward and down looking cameras, which doesn't rely on the assumption of level flight. First, the distribution and decoupling method of optical flow from forward camera are utilized to get attitude. Then, the resulted angular velocities are utilized to obtain the translational optical flow of the down camera, which can eliminate the influence of rotational motion on velocity estimation. Besides, the translational motion estimation equation is simplified by establishing the relation between the depths of feature points and the aircraft altitude. Finally, simulation results show that the method presented is accurate and robust.展开更多
This paper investigates the six degree-of-freedom(6DOF)relative kinodynamic motion planning problem for spacecraft close approach operations,wherein a controlled chaser spacecraft is required to approach a noncooperat...This paper investigates the six degree-of-freedom(6DOF)relative kinodynamic motion planning problem for spacecraft close approach operations,wherein a controlled chaser spacecraft is required to approach a noncooperative space target at a close range under both dynamic constraints and motion constraints.An enhanced version of the bidirectional rapidlyexploring random tree^(*)(BiRRT^(*))algorithm based on flight zoning(FZ-BiRRT^(*))is proposed to generate safe,feasible,and nearoptimal relative motion trajectories.In the proposed algorithm,the space surrounding the space target is zoned in a spherical coordinate system based on the collision probability so that specific designs can be made for different phases of the approaching.Subsequently,based on the flight zone,dynamic constraints,and experiential knowledge,a series of modifications are made to the classic BiRRT^(*)algorithm,and a postprocessing step is designed to accelerate convergence and promote search efficiency.Furthermore,a general regression neural network is introduced to fit a smooth and applicable final motion trajectory.Finally,the feasibility of the generated motion trajectory and the superiority of the proposed algorithm is demonstrated by means of numerical simulations.展开更多
A roll-decoupled course correction fuze with canards can improve the hit accuracy of conventional unguided ammunitions. The fuze increases accuracy by reducing the effect of angular and translational motion produced b...A roll-decoupled course correction fuze with canards can improve the hit accuracy of conventional unguided ammunitions. The fuze increases accuracy by reducing the effect of angular and translational motion produced by the cyclical yawing forces applied on the projectile. In order to investigate the influence of yawing forces on angular motion, a theoretical solution of the total yaw angle function with the cyclical yawing forces is deduced utilizing the 7 degrees of freedom(7-DOF) model designed for this calculation. Furthermore, a detailed simulation is carried out to determine the influence rules of yawing force on angular motion. The calculated results illustrate that, when the rotational speed of the forward part is close to the initial turning rate, the total yaw angle increases and the flight range decreases sharply. Moreover, a yawing force at an appropriate frequency is able to correct the gun azimuth and elevation perturbation to some extent.展开更多
文摘针对船体密封舱、箱柜等狭窄空间普遍存在的机器人难以工作问题,提出了一种新型6-DOF(degrees of freedom)机器人。首先分析了该机器人的机械结构,基于D-H坐标理论建立了机器人D-H坐标表格以及机器人正、逆运动学方程,其次应用MATLAB对机器人的运动学进行了仿真,结果表明所得的机器人正、逆运动学方程完全正确;最后设计了虚拟样机,利用RobotStudio仿真分析了机器人箱体焊接的优点;为进一步验证设计的机器人运动性能,与通用6-DOF机器人做了对比分析。研究结果表明新型机器人运动的可行性,为设计适应箱柜等狭窄空间的工业机器人提供了理论依据。
基金Project(2012CB720003)supported by the National Basic Research Program of ChinaProjects(61320106010,61127007,61121003,61573019)supported by the National Natural Science Foundation of ChinaProject(2013DFE13040)supported by the Special Program for International Science and Technology Cooperation from Ministry of Science and Technology of China
文摘Because of its characteristics of simple algorithm and hardware, optical flow-based motion estimation has become a hot research field, especially in GPS-denied environment. Optical flow could be used to obtain the aircraft motion information, but the six-(degree of freedom)(6-DOF) motion still couldn't be accurately estimated by existing methods. The purpose of this work is to provide a motion estimation method based on optical flow from forward and down looking cameras, which doesn't rely on the assumption of level flight. First, the distribution and decoupling method of optical flow from forward camera are utilized to get attitude. Then, the resulted angular velocities are utilized to obtain the translational optical flow of the down camera, which can eliminate the influence of rotational motion on velocity estimation. Besides, the translational motion estimation equation is simplified by establishing the relation between the depths of feature points and the aircraft altitude. Finally, simulation results show that the method presented is accurate and robust.
基金supported by the Science Center Program of National Natural Science Foundation of China(62188101)the National Key Research and Development Program of China(2024YFF0504702)the SiYuan Collaborative Innovation Alliance of Artificial Intelligence Science(HTKJ2023SY502003).
文摘This paper investigates the six degree-of-freedom(6DOF)relative kinodynamic motion planning problem for spacecraft close approach operations,wherein a controlled chaser spacecraft is required to approach a noncooperative space target at a close range under both dynamic constraints and motion constraints.An enhanced version of the bidirectional rapidlyexploring random tree^(*)(BiRRT^(*))algorithm based on flight zoning(FZ-BiRRT^(*))is proposed to generate safe,feasible,and nearoptimal relative motion trajectories.In the proposed algorithm,the space surrounding the space target is zoned in a spherical coordinate system based on the collision probability so that specific designs can be made for different phases of the approaching.Subsequently,based on the flight zone,dynamic constraints,and experiential knowledge,a series of modifications are made to the classic BiRRT^(*)algorithm,and a postprocessing step is designed to accelerate convergence and promote search efficiency.Furthermore,a general regression neural network is introduced to fit a smooth and applicable final motion trajectory.Finally,the feasibility of the generated motion trajectory and the superiority of the proposed algorithm is demonstrated by means of numerical simulations.
文摘A roll-decoupled course correction fuze with canards can improve the hit accuracy of conventional unguided ammunitions. The fuze increases accuracy by reducing the effect of angular and translational motion produced by the cyclical yawing forces applied on the projectile. In order to investigate the influence of yawing forces on angular motion, a theoretical solution of the total yaw angle function with the cyclical yawing forces is deduced utilizing the 7 degrees of freedom(7-DOF) model designed for this calculation. Furthermore, a detailed simulation is carried out to determine the influence rules of yawing force on angular motion. The calculated results illustrate that, when the rotational speed of the forward part is close to the initial turning rate, the total yaw angle increases and the flight range decreases sharply. Moreover, a yawing force at an appropriate frequency is able to correct the gun azimuth and elevation perturbation to some extent.
