This paper deals with the issue of preparation of the aiming angles with the use of tabular firing tables and needed determination of the ballistic elements μ_B(ballistic wind w_B,w_(xB),w_(ZB),ballistic(virtual) tem...This paper deals with the issue of preparation of the aiming angles with the use of tabular firing tables and needed determination of the ballistic elements μ_B(ballistic wind w_B,w_(xB),w_(ZB),ballistic(virtual) temperature τ_B.ballistic density p_B) from the standardized met messages.The weighting factors are used for the calculation of ballistic elements μ_B that are incorporated into the trajectory calculations characteristics of weapon and ammunition.Two different methodologies practically used in the praxis are analysed and compared.For the comparison of the two methodologies the reference height of trajectory determined from the weighting factor functions is employed.On the basis of the analyses conducted,the potential for further increase in accuracy of these aiming angles preparation methods is pointed out.展开更多
In order to make motion planning fitting practice,many characteristic of CNC trajectory motion are discussed, such as the geometric function,the motion and the time.It is found that the relation between orbit function...In order to make motion planning fitting practice,many characteristic of CNC trajectory motion are discussed, such as the geometric function,the motion and the time.It is found that the relation between orbit function and motional parame- ter,so the differential equation about the trajectory motion be set-up by the goal of trajectory motion.The actual motion process is defined as reference time to link planning and practice.Present a new movement planning method based on self-defining time.At rest state,the differential simultaneous equation can be calculated according geometric characteristic analysis,it can be get that simple function consisted of coordinate and reference time variants.At motive state,dynamic parameter can be worked out accord- ing practical value of reference time,It is proved by experiment and simulation that it is a good way to control geometry and motion comprehensively,to reduce computation times and to increase the ability of environmental adaptation for path展开更多
Projectile trajectories calculated under non-standard conditions are considered to be perturbed. The tools utilized for the analysis of perturbed trajectories are weighting factor functions(WFFs) which are a special k...Projectile trajectories calculated under non-standard conditions are considered to be perturbed. The tools utilized for the analysis of perturbed trajectories are weighting factor functions(WFFs) which are a special kind of sensitivity functions. WFFs are used for calculation of meteo ballistic elements mB(ballistic wind wB, virtual temperature tB, pressure pB, density rB, speed of sound a) as well. An effect of weapon system parameters can be incorporated into calculations through the reference height of trajectory-RHT.RHT are also calculated from WFFs. Methods based on RHT are far more effective than traditional methods that use weighting factors q.We have found that the existing theory of RHT has several shortcomings due to we created an improved theory of generalized RHT which represent a special sensitivity parameters of dynamical systems. Using this theory will improve methods for designing firing tables, fire control systems algorithms, and meteo message generation algorithms.展开更多
文章以插电式混合动力汽车(plug-in hybrid electric vehicle,PHEV)为研究对象,以提高整车燃油经济性和排放性能为目标,设计了能够实现需求转矩在发动机和驱动电机之间合理分配的模糊逻辑控制策略。该模糊控制策略以SOC参考轨迹作为切入...文章以插电式混合动力汽车(plug-in hybrid electric vehicle,PHEV)为研究对象,以提高整车燃油经济性和排放性能为目标,设计了能够实现需求转矩在发动机和驱动电机之间合理分配的模糊逻辑控制策略。该模糊控制策略以SOC参考轨迹作为切入点,最大程度地发挥动力电池的存储能量。仿真结果表明,该模糊控制策略能够较好地优化发动机工作区间,提高燃油经济性和排放性能,并且能使动力电池SOC保持在设定的参考轨迹附近波动。展开更多
研究了重复使用运载器(reusable launch vehicle,RLV)末端能量管理段(terminal area energy manage-ment,TAEM)三维制导轨迹推演算法。根据初始点和终点的位置、航向、动压,规划动压参考剖面和横侧向参考轨迹,采用基于高度的质点动力学...研究了重复使用运载器(reusable launch vehicle,RLV)末端能量管理段(terminal area energy manage-ment,TAEM)三维制导轨迹推演算法。根据初始点和终点的位置、航向、动压,规划动压参考剖面和横侧向参考轨迹,采用基于高度的质点动力学方程推演生成符合过载、动压、终点位置和航向约束条件的三维制导轨迹。横侧向参考轨迹的设计可以分成两步:第一步,消除横向的位置误差,同时减小纵向的位置误差;第二步,消除纵向的位置误差。根据纵向位置误差大小,组合使用三种模态的轨迹予以消除,节省了计算量。仿真计算显示,三维制导轨迹推演算法具有快速、准确、对初始点位置和航向分布鲁棒性强的特点,为在线轨迹设计提供了基础算法。展开更多
基金support of financial means from the industrial research project of the Ministry of the Interior of the Czech Republic-project code VG20122015076:"Two survey points range-finding system utilization for perimeter security(screen)"the Research project for the development of the Department of Weapons and Ammunition,Faculty of Military Technology, University of Defence,Brno,PRO K-201
文摘This paper deals with the issue of preparation of the aiming angles with the use of tabular firing tables and needed determination of the ballistic elements μ_B(ballistic wind w_B,w_(xB),w_(ZB),ballistic(virtual) temperature τ_B.ballistic density p_B) from the standardized met messages.The weighting factors are used for the calculation of ballistic elements μ_B that are incorporated into the trajectory calculations characteristics of weapon and ammunition.Two different methodologies practically used in the praxis are analysed and compared.For the comparison of the two methodologies the reference height of trajectory determined from the weighting factor functions is employed.On the basis of the analyses conducted,the potential for further increase in accuracy of these aiming angles preparation methods is pointed out.
基金Supported by the Natural Science Foundation of Education Committee of Sichuan Province(2004A163)
文摘In order to make motion planning fitting practice,many characteristic of CNC trajectory motion are discussed, such as the geometric function,the motion and the time.It is found that the relation between orbit function and motional parame- ter,so the differential equation about the trajectory motion be set-up by the goal of trajectory motion.The actual motion process is defined as reference time to link planning and practice.Present a new movement planning method based on self-defining time.At rest state,the differential simultaneous equation can be calculated according geometric characteristic analysis,it can be get that simple function consisted of coordinate and reference time variants.At motive state,dynamic parameter can be worked out accord- ing practical value of reference time,It is proved by experiment and simulation that it is a good way to control geometry and motion comprehensively,to reduce computation times and to increase the ability of environmental adaptation for path
基金the Research Project for the Development of the Department of Weapons and Ammunition, Faculty of Military Technology, University of Defence, Brno, DZRO VYZBROJ
文摘Projectile trajectories calculated under non-standard conditions are considered to be perturbed. The tools utilized for the analysis of perturbed trajectories are weighting factor functions(WFFs) which are a special kind of sensitivity functions. WFFs are used for calculation of meteo ballistic elements mB(ballistic wind wB, virtual temperature tB, pressure pB, density rB, speed of sound a) as well. An effect of weapon system parameters can be incorporated into calculations through the reference height of trajectory-RHT.RHT are also calculated from WFFs. Methods based on RHT are far more effective than traditional methods that use weighting factors q.We have found that the existing theory of RHT has several shortcomings due to we created an improved theory of generalized RHT which represent a special sensitivity parameters of dynamical systems. Using this theory will improve methods for designing firing tables, fire control systems algorithms, and meteo message generation algorithms.
文摘文章以插电式混合动力汽车(plug-in hybrid electric vehicle,PHEV)为研究对象,以提高整车燃油经济性和排放性能为目标,设计了能够实现需求转矩在发动机和驱动电机之间合理分配的模糊逻辑控制策略。该模糊控制策略以SOC参考轨迹作为切入点,最大程度地发挥动力电池的存储能量。仿真结果表明,该模糊控制策略能够较好地优化发动机工作区间,提高燃油经济性和排放性能,并且能使动力电池SOC保持在设定的参考轨迹附近波动。
文摘研究了重复使用运载器(reusable launch vehicle,RLV)末端能量管理段(terminal area energy manage-ment,TAEM)三维制导轨迹推演算法。根据初始点和终点的位置、航向、动压,规划动压参考剖面和横侧向参考轨迹,采用基于高度的质点动力学方程推演生成符合过载、动压、终点位置和航向约束条件的三维制导轨迹。横侧向参考轨迹的设计可以分成两步:第一步,消除横向的位置误差,同时减小纵向的位置误差;第二步,消除纵向的位置误差。根据纵向位置误差大小,组合使用三种模态的轨迹予以消除,节省了计算量。仿真计算显示,三维制导轨迹推演算法具有快速、准确、对初始点位置和航向分布鲁棒性强的特点,为在线轨迹设计提供了基础算法。
