共查询到17条相似文献,搜索用时 62 毫秒
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针对水下滑翔机运动过程中的特点,水下滑翔机实际运动过程可以分为定常运动段和非定常运动段,对自设计的水下滑翔机原理样机建立了基于单刚体六自由度的定常运动段的数学模型并进行了数值仿真,在此基础上分别对水下滑翔机运动过程中的两种定常运动—直线定常运动和螺旋定常运动进行了分析。结论显示在直线定常运动中俯仰角和攻角随平移质量块位置的增大先变化迅速后变化缓慢。滑翔角随平移质量块位置的增大近似呈线性增大的关系。在螺旋定常运动中通过模型仿真得到螺旋运动特征参数(螺旋半径、螺旋线螺距、螺旋时间周期、速度)和状态参数(滑翔角、翻滚角、各方向速度分量、各方向角速度分量),根据最小二乘法拟合得到它们之间的关系,从而说明了螺旋运动状态是如何通过调整平移质量块移动距离,旋转质量块旋转角度和净重力等控制量而变化的。 相似文献
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随着对水下机器人研究的逐步深入,其运动能力已由早期单纯的平动逐步强化为有多个自由度的空间运动,对其进行动力学研究是进行其它方面能力研究的基础。为研究多自由度水下机器人的运动,对某型八推进器水下机器人进行了动力学方程建模,得出了其在6个自由度上的运动方程,在此基础上,对其进行了运动仿真及性能分析,得到了该型水下机器人在6个自由度上的运动性能。通过仿真计算的结果,可以直观地了解其运动能力。 相似文献
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对水下滑翔器的整体外形设计与水动力性能进行研究。在Slocum等几种典型水下滑翔器样机的基础上,对滑翔器的主体和附体进行一体化设计,得到阻力最小的新型水下滑翔器构型设计。利用CFD方法对水下滑翔器进行模拟仿真,通过分析对比五种主体构型,得到了比较合理的主体线型,然后用正交设计方法和曲线拟合法对附体进行了优选工作,最后得到了性能更优的整体载体外形。模拟仿真实验表明,滑翔器在8°左右攻角航行时,具有最大的升阻比;和Slocum等经典样机相比,新的载体具有更好的水动力性能。通过上述研究工作,也可以缩短水下滑翔器研制周期,降低设计成本,并为水下滑翔器的更优设计提供了有力的技术指导和参考。 相似文献
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对水下滑翔机器人SEA-WING的定常滑翔运动和空间定常螺旋回转运动进行机理分析,针对其特定水动力系数进行仿真,得出其运动机理特性.在此基础上,通过湖试实验数据对仿真结果进行验证,认为对于定常滑翔运动,以约36°航迹角滑行可得到最大水平速度;在相同航迹角航行情况下,水平方向速度随净浮力的增大而增大.对于定常回转运动,回转半径由载体的质量、俯仰角、水动力参数、横滚角确定.在质量和俯仰角保持不变条件下,横滚角对回转半径的影响较明显,系统的回转半径可以通过控制横滚角来实现的. 相似文献
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分析大深度潜航器水下空间运动特点,建立描述其空间运动的数学模型,并以数学模型为基础利用MATLABSimulink软件完成潜航器空间运动仿真模型的开发.在搭建的仿真模型基础上,通过数学仿真手段分析了潜航器在螺旋下潜、抛载过渡、定角爬升、稳定至水面航行状态下的水下运动全过程,给出了具有弧形翼板的潜航器外形设计方案的运动... 相似文献
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For consideration of both the eccentric rotatable rigid body and the translational rigid body, the dynamic model of the underwater glider is derived. Dynamical behaviors are also studied based on the model and can be used as the guidance to underwater gliders design. Gibbs function of the underwater glider system is derived first, and then the nonlinear dynamic model is obtained by use of Appell equations. The relationships between dynamic behaviors and design parameters are studied by solving the dynamic m... 相似文献
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Dynamic Analysis of Towed and Variable Length Cable Systems 总被引:2,自引:3,他引:2
Towed cable systems are frequently used in marine measurements where the length of the towed cable varies during launch and recovery. In this paper a novel method for modeling variable length cable systems is introduced based on the finite segment formulation. The variable length of the towed cable is described by changing the length of the segment near the towing point and by increasing or decreasing the number of the discrete segments of the cable. In this way, the elastic effects of the cable can be easily handled since geometry and material properties of each segment are kept constant. Experimental results show that the dynamic behavior of the towed cable is consistent between the model and the physical cable. Results show that the model provides numerical efficiency and simulation accuracy for the variable length towed system. 相似文献
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PETREL,a winged hybrid-driven underwater glider is a novel and practical marine survey platform which combines the features of legacy underwater glider and conventional AUV (autonomous underwater vehicle).It can be treated as a multi-rigid-body system with a floating base and a particular hydrodynamic profile.In this paper,theorems on linear and angular momentum are used to establish the dynamic equations of motion of each rigid body and the effect of translational and rotational motion of internal masses on the attitude control are taken into consideration.In addition,due to the unique external shape with fixed wings and deflectable rudders and the dual-drive operation in thrust and glide modes,the approaches of building dynamic model of conventional AUV and hydrodynamic model of submarine are introduced,and the tailored dynamic equations of the hybrid glider are formulated.Moreover,the behaviors of motion in glide and thrust operation are analyzed based on the simulation and the feasibility of the dynamic model is validated by data from lake field trials. 相似文献
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For Cconsideration ofing both the eccentric rotatable rigid body and the translational rigid body, the dynamic model of the underwater glider is derived. Dynamical behaviors are also studied based on the model and can be used as the guidance to underwater gliders design. Gibbs function of the underwater glider system is derived first, and then the nonlinear dynamic model is obtained by use of Apell Equations. The relationships between dynamical behaviors and design parameters are studied by solving the dynamic model. The spiral motion, swerving motion in three dimensions and the saw-tooth motion of the underwater glider in vertical plane are studied. Lake trials are carried out to validate the dynamic model. 相似文献
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Development and experiments of the Sea-Wing underwater glider 总被引:1,自引:0,他引:1
Underwater gliders,which glide through water columns by use of a pair of wings,are efficient long-distance,long-duration marine environment observatory platforms.The Sea-Wing underwater glider,developed by the Shenyang Institute of Automation,CAS,is designed for the application of deep-sea environment variables observation.The system components,the mechanical design,and the control system design of the Sea-Wing underwater glider are described in this paper.The pitch and roll adjusting models are derived based on the mechanical design,and the adjusting capabilities for the pitch and roll are analyzed according to the models.Field experiments have been carried out for validating the gliding motion and the ability of measuring ocean environment variables.Experimental results of the motion performances of the glider are presented. 相似文献
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The flying-wing underwater glider (UG), shaped as a blended wing body, is a new type of underwater vehicle and still requires further research. The shape layout and the configuration of the internal actuators of the flying-wing UG are different from those of \"legacy gliders\" which have revolving bodies, and these two factors strongly affect the dynamic performance of the vehicle. Considering these differences, we propose a new configuration of the internal actuators for the flying-wing UG and treat the flying-wing UG as a multi-body system when establishing its dynamic model. In this paper, a detailed dynamic model is presented using the Newton-Euler method for the flying-wing UG. Based on the full dynamic model, the effect of the internal actuators on the steady gliding motion of vehicle is studied theoretically, and the relationship between the state parameters of the steady gliding motion and the controlled variables is obtained by solving a set of equilibrium equations. Finally, the behaviors of two classical motion modes of the glider are analyzed based on the simulation. The simulation results demonstrate that the motion performance of the proposed flying-wing UG is satisfactory. 相似文献