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航天员舱外活动安全绳虚拟现实操作仿真方法研究 总被引:1,自引:0,他引:1
《载人航天》2018,(6)
为了解决航天员舱外活动虚拟现实训练仿真中安全绳的逼真仿真问题,分析了安全绳的结构组成和神七任务航天员出舱过程微重力下的安全绳变形规律,对安全绳采用质点-直线弹簧-弯曲弹簧模型建模,使用基于位置的仿真方法计算了安全绳的变形,给出了安全绳的仿真参数,建立了航天员舱外活动安全绳操作仿真系统。开展了受试者试验,仿真结果表明,仿真方法实时有效,可为航天员虚拟现实舱外维修仿真提供基础算法。 相似文献
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舱外航天服手套加热方案探讨 总被引:4,自引:0,他引:4
针对舱外作业中航天员常常因手冷而不得不提前回舱的情况,提出了主动加热的方法。利用边界元法以边界点上未知函数满足积分方程为基础进行近似计算的特点,建立了手部和舱外航天服手套温度场三维计算模型,通过模拟试验件验证了模型。模型针对航天员处于太阳和地球辐射阴面时提出了舱外航天服手套主动加热的优化方案,并通过模拟试验件验证加热方法合理。 相似文献
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Asker JR 《Aviation week & space technology》1995,143(3):40-43
U.S. astronauts and Russian cosmonauts both use space suits when performing extravehicular activity (EVA), but these have been developed independently due to the diverse goals of each country's space program. The current versions of the U.S. and Russian space suits were compared when the author tested both suits on the same day. The similarities and differences are noted, as well as the strengths and limitations of each. Determination of the compatibility of these suits is important as increased cooperation between the U.S. and Russia has occurred (for example, astronauts and cosmonauts are flying together on Shuttle/Mir missions) and as the international space station becomes reality. 相似文献
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重装空投动力学分析与控制方案研究 总被引:1,自引:0,他引:1
针对重装空投任务,基于拉格朗日分析力学,建立了货物在机舱内滑行阶段飞机-货物两体系统的动力学模型.给出了一种控制补偿方案,用以抵消或削弱货物运动对飞机的影响.通过数值仿真,观察货物运动和飞机运动之间的耦合关系,分析了牵引伞尺寸对飞机和货物运动参数的影响.仿真结果表明,所给出的控制补偿方案能够有效改善飞机飞行品质,提高飞... 相似文献
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对环月轨道共面交会的载人登月任务中,着陆器(LM)奔月零窗口与轨道参数精确快速设计方法进行了研究。任务采用人货分离奔月模式,着陆器于载人飞船到达环月轨道前抵达环月共面交会轨道,着陆器近月点一次共面减速完成近月制动。提出一种三层快速精确奔月窗口搜索方法:第一层采用地心二体轨道理论解析计算月窗口及奔月轨道参数初值,作为正确性基本参考;第二层采用改进的双二体解析动力学模型求解月窗口内奔月轨道参数变化规律;第三层采用高精度轨道动力学模型和SQP_Snopt优化求解奔月零窗口及轨道参数精确解。仿真结果表明,本文提出的三层逐级奔月窗口搜索方法能快速精确求解载人登月任务中着陆器奔月窗口及精确轨道参数,也揭示了影响着陆器奔月窗口的主次因素和规律,为中国未来载人登月工程提供参考。 相似文献
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《中国航空学报》2023,36(3):436-448
Bolt assembly by robots is a vital and difficult task for replacing astronauts in extra-vehicular activities (EVA), but the trajectory efficiency still needs to be improved during the wrench insertion into hex hole of bolt. In this paper, a policy iteration method based on reinforcement learning (RL) is proposed, by which the problem of trajectory efficiency improvement is constructed as an issue of RL-based objective optimization. Firstly, the projection relation between raw data and state-action space is established, and then a policy iteration initialization method is designed based on the projection to provide the initialization policy for iteration. Policy iteration based on the protective policy is applied to continuously evaluating and optimizing the action-value function of all state-action pairs till the convergence is obtained. To verify the feasibility and effectiveness of the proposed method, a noncontact demonstration experiment with human supervision is performed. Experimental results show that the initialization policy and the generated policy can be obtained by the policy iteration method in a limited number of demonstrations. A comparison between the experiments with two different assembly tolerances shows that the convergent generated policy possesses higher trajectory efficiency than the conservative one. In addition, this method can ensure safety during the training process and improve utilization efficiency of demonstration data. 相似文献
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通过建立由等离子体声源、PCB压力传感器和高速相机等构成的实验测量系统,研究了强声波脉冲引发的空化气泡运动和二次声辐射。通过实验,观察到了强声波脉冲特有的波形结构,空化气泡的成长、膨胀和坍缩过程以及气泡坍缩时辐射的声信号。其次,利用Gilmore方程和Bernoulli方程,从理论上对空化气泡的运动和声辐射进行了数值模拟和分析。研究结果表明:(1)在强声波脉冲正压区的作用下,空化气泡将受到压缩并围绕"准平衡态半径"振荡;在强声波脉冲负压区的作用下,空化气泡将出现膨胀、坍缩和回弹的物理过程。(2)空化气泡坍缩时周期性辐射的声脉冲持续时间极短,具有"冲击波"的特点。 相似文献
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设计开发了MSVAS(建模与仿真VV&A(校核、验证和确认)辅助软件),提高导弹动力学仿真系统VV&A自动化程度。过程管理模块通过工程配置文件设计,提供VV&A流程的图形化设计与管理、任务安排等功能,指导VV&A工作顺利进行;评估分析模块提供方法库,为各类具体评估工作提供技术方法支持;模型测试模块提供各种试验设计方法,目的是为充分测试评估模型的可信性设计各类测试实例;资源管理模块对导弹动力学系统VV&A所涉及到的数据、模型和文档等资源进行了合理、有效的管理。MSVAS能为导弹动力学仿真系统VV&A提供过程管理、技术等支持,提高了VV&A工作效率,并减轻工作者的负担。 相似文献