Research on application of virtual guidance to the trajectory optimization of reentry-glide flight

A Method of Trajectory Optimization for Homing Antiaircraft Missile

寻的防空导弹的一种弹道优化方法

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The optimum longitudinal glide trajectory design for general air-to-ship missile was discussed.

本文对一般空舰导弹的纵向下滑段弹道优化设计进行了探讨；

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Optimum Design of Climb Trajectory for a Cruise Missile

巡航导弹加速爬升段弹道优化设计

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Optimization Design of Reentry Trajectory for Maneuverable Warhead Based on Genetic Algorithms

基于遗传算法的机动弹头再入段弹道优化设计

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Optimal study on the underwater weapon's interior trajectory of compressed-air launcher

气动式水下武器发射器内弹道优化研究

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Application of Improved Real-coded Genetic Algorithm in Interior Ballistic Optimization

改进型实数编码遗传算法在内弹道优化中的应用

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Study of Trajectory Optimization and Guidance Algorithm for Boost-Glide Missile

助推&滑翔导弹弹道优化与制导方法研究

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The exterior ballistic optimum design for anti-aircraft projectiles of small calibers

小口径高炮弹丸外弹道优化设计

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Trajectory optimization using Collocation Based on high order Gauss lobatto quadrature rules

用高精度配点法进行弹道优化

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The results show that it is content with exponential burning rate law. Based on the experiment data, the burning rate coefficient and exponent were adapted. The research results can give basic data for the interior ballistic design of the liquid propulsion system.

结果表明，它满足指数燃速定律，并从试验数据拟合出燃速系数和燃速指数，其结果可为液体推进系统内弹道设计提供基础数据。

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Based on analyzing test data of intercepting air-to-surface and surface-to-surface tactics missile, the evaluation method of kill effect of intercepting tactics missile was presented.

拦截战术导弹杀伤效果的评定方法，在分析拦截战术弹道导弹的试验数据基础上提出。

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Data fusing to trajectory tracking system

弹道跟踪系统的数据融合

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Study of the analyzing method on interior ballistic multi-channel pressure histories

内弹道多通道实验数据处理方法研究

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Data Interpretation of the Dumping Cruise Data Recorder A NEW METHOD FOR IMAGE ANALYSIS AND DATA EXTRACTION OF PROJECTILES IN FLIGHT

倾废航行数据记录仪的数据判读弹道靶道数据判读与处理方法研究

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A New Algorithm for Data Fusion of the Trajectory Computing Only with the Velocity and Its Application

全测速测元弹道计算的数据融合算法与应用

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Based on Fractal Brownian Motion ( FBM) model, tracking residual data for vehicle is processed.

利用分数（形）布朗运动（FBM）模型，分析了飞行器弹道测量误差数据的分形特性；

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A nonlinear fusion model on the ITM ETM data is established in the velocity domain in inertial coordinate system ( ICS), using the ITM presented by control system error ( CSE) coefficients and the differential equation connecting the ITM and the ETM.

在惯性坐标系的速度域上，通过内弹道测量数据和控制系统误差系数表示内弹道及联系内外弹道的微分方程，建立了基于内外弹道测量数据的非线性融合参数模型。

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Theoretical analysis and simulation calculations clearly show that the model is accuracy, the parameter estimation methods in question possess high accuracy, applying the methods can improving the quantity of observation data.

理论分析和仿真计算表明：本文所建的模型准确，参数估计方法精度高，应用本文方法能明显提高弹道跟踪数据质量。

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This paper brings forward a speedy method for trajectory recognition based on the minimum of trajectory velocity by analyzing a great deal of datum, and proves its correctness abstractly.

通过对大量弹道仿真数据的分析，提出了基于弹道速度最小点的弹道辩识快速算法，并从理论上证明了该算法的正确性。

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The paper presents the application of cumulative-sum method in the field of external trajectory measurement data processing to fit ballistic trajectory and estimate missiles velocity parameters.

文中提出将累积法应用到外弹道测量数据处理中，用以拟合导弹的飞行轨迹，估计导弹飞行的速度参数。

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