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A new accurate exterior trajectory model was studied based on the formertrajectory model considering eccentricity of acceleration of gravity etc.

本文在已有弹道数学模型的基础上,研究了地球为椭球体时重力偏心,全面考虑了重力偏心及以往在射程和弹道高不大时忽略的"小量",建立了高空远程弹箭的较精确弹道数学模型。

This paper describes the basic principle of velocity pursuit guidance law and body pursuit guidance law of trajectory correction projectiles , researches the terminal correction trajectory and miss distance under pursuit guidance laws by 6—DOF trajectory simulation program, researches the orbit of laser detector ray axis and ground projection area of laser detector spatial viewpoint.

文中对速度追踪制导律和弹体追踪制导律的工作原理进行了研究,利用六自由度弹道仿真程序对弹道修正弹两种追踪方式下的末段修正弹道和脱靶量进行了对比计算,研究了两种追踪方式下激光探测器光轴的轨迹及激光探测器空间视场在地面投影区域的变化;弹体追踪方式命中精度虽然较低,但由于工程实现简单、成本低,仍有其工程使用价值。

According to the missile simulation data, mapping can be visual display characteristics of an ideal ballistic ballistic curve.

详细说明:根据导弹仿真数据,绘制可直观显示弹道特性的理想弹道曲线。

The result shows that the canard parameters and angular velocity are the main factors which influence the dynamic stability of the controllable projectile and should be controlled reasonably in the process of the design of aerodynamic configuration and trajectory.

结果表明,舵面参数与弹丸转速是影响有控弹道动稳定的主要因素,须在气动布局参数设计和弹道设计时加以合理控制。

In order to meet the required simulation precision and meet the real-time simulation in ballistic simulation calculation,this paper analyzes the selection method of the simulation step,and then introduces variable step integration methods in Runge-Kutta to Adams and educes Adams variable step integral formulas,and then put forwards a method by seeking zero of condition function in discontinuous nonlinear system of the ballistic simulation.

在弹道仿真计算中,为了既达到要求的仿真精度又能满足实时仿真,分析了仿真步长的选择方法,然后在龙格-库塔转阿当姆斯法中引入变步长积分方法,推导了阿当姆斯变步长积分公式,同时对弹道仿真中的间断非线性系统提出条件函数求零的方法来解算弹道。

On the basis of shock wave characteristic of the supersonic projectile and the detailed analysis of measured datas,a method of decomposing and reconstructing the trajectory shock wave signal and muzzle blast wave signal is proposed and the characteristic parameters for positioning sound source and calculating trajectory vector with regular tetrahedron detection array are extracted.

根据空气动力学原理,在阐述超音速弹丸的弹道波特性的基础上,通过详细分析实测的声信号,提出了弹道波信号和枪口冲击波信号的小波分解和重构方法,提取了利用正四面体探测基阵进行声源定位和弹道矢量计算的特征参数,获得了满意的实验结果。

This article expatiates and argumentations contents as follow: background and meaningof study the task, basis concept of system simulation, technology of seeable, the theory of inner trajectory and test data analysis, inner trajectory numerical value simulation and test result analysis, computer simulation analysis system of shell in internal ballistic test, technology exploitation scheme of 3D simulation software and so on.

本文对研究课题的背景及意义、系统模拟仿真的基本概念、可视化、内弹道模型与试验数据分析理论、内弹道数值模拟与试验结果分析、炮弹内弹道试验计算机仿真系统、三维仿真软件开发技术方案等内容进行了阐述和论证。

The results show that under the complicated upper limit control logic,the upper limit depth trajectory is not a simple form,but two or more irregular forms of re-entering into the upper limit depth,or regular oscillation form around the upper limit depth.These results may be expected to provide a theoretical basis for analyzing the problem in sea trial.

仿真结果表明,在复杂的上限控制逻辑下,上限深度弹道不是一种形式,可能存在不规则的2次或多次再进入上限的弹道形式,或者存在上限附近深度规则振荡的弹道形式,这些规律为实航中出现的一些特殊现象分析提供了理论依据。

In order to improve penetrativity of hypersonic missile and enable air-launched hypersonic cruise missile to penetrate with skip trajectory, a new approach of generating positive angle of attack during reentry phase of trajectory was proposed. Some key parameters of realizing skip trajectory were found out, and the effects of these parameters on ballistic performance were discussed.

为提高高超声速导弹的突防能力,使常规布局空中发射的高超声速巡航弹能采用跳跃式弹道突防,采用了在导弹再入段附加相应的正攻角产生气动升力的方法,找出了实现弹道起跳的关键参数,讨论了这些参数对弹道性能的影响。

Though we have make much progress on it, there remains many problems to study deeply, of which its supporting software system developing is an important and elementary subject of torpedo trajectory research.In this article, we bring forward the double-color method for stereodisplay of the torpedos trajectory.

在鱼雷弹道研究方面已经取得了可喜的成果,但仍不能满足鱼雷事业新发展的要求,需要深入研究的问题还很多,其中鱼雷弹道软件系统的开发仍是鱼雷弹道研究中的一项重要而又基础性的课题。

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