高超声速飞行器俯冲机动最优制导方法

为解决高超声速飞行器俯冲段精确制导与机动突防问题,研究了机动突防最优制导方法。针对零化视线角速率降低突防性能的问题,在俯冲平面及转弯平面内分别设计了正弦形式的视线角参考运动,同时为进一步实现俯冲精确制导,以落速最大为性能指标利用最优控制对其进行跟踪,引入了伪控制量以简化最优制导问题的求解,最后分析了该方法的稳定性及制导性能。以CAV-H为例进行仿真分析,仿真结果表明该方法能够实现机动飞行,且能够高精度地满足终端落角及落点约束,可为高超声速飞行器俯冲段精确制导及机动突防提供参考。     

基于NMPC的战斗机末端机动规避策略

利用非线性模型预测控制（nonlinear model predictive control,NMPC）的思想建立了战机末端规避导弹的机动策略求解方法。根据导弹与战机的空战态势,建立了导弹与战机的相对运动微分方程;将导弹的导引律引入到导弹运动模型中,与飞机模型一起构建了系统预测模型,并对飞机和导弹的运动约束进行了分析。通过对导弹结构限制和战术特性的分析,给出了飞机机动规避导弹的性能指标,进而建立了机动规避导弹的最优控制模型。利用高斯伪谱法对模型进行求解,采用滚动优化策略实现了对机动规避策略的闭环求解。针对导弹气动参数和导航比未知以及相对测量量具有噪声的问题,利用极大似然法对导弹的气动参数和导航比进行估计,实现了对系统预测模型的反馈校正。仿真结果表明,此方法能够实现对导弹的机动规避。     

再入机动弹头的速度控制

本文详细地讨论了再入机动弹头的速度控制问题。根据优化原理找到了对固定目标进行攻击的最优制导规律,讨论了理想速度曲线的设计方法,以及具体实施减速控制的方法。仿真计算表明,对落速控制的精度是较高的。     

Satellite constellation design for forest fire monitoring via a stochastic programing approach

There is significant value in the data collected by satellites during and after a natural disaster. The current operating paradigm in practice is for satellites to passively collect data when they happen to fly over a disaster location. Conversely, this article considers the alternative approach of actively maneuvering satellites to fly directly overhead of the disaster site on a routine basis. Toward this end, we seek to compute a satellite constellation design that minimizes the expected maneuver costs for monitoring an unknown forest fire. In this article, we present a 2‐stage stochastic programing model for this problem as well as a accelerated L‐shaped decomposition approach. A comparison between our approach and the current operating paradigm indicates that our solution provides longer duration data collections and a greater number of data collections. Analysis also shows that our proposed solution is robust over a wide array of scenarios.     

基于层次化的SVDDBNs的多机动平台目标分配方式

针对天基机动平台集群作战时的目标分配问题。提出一种基于层次化思想的变结构离散动态贝叶斯网络(SVDDBNs)的平台-目标分配方式。首先提出了目标分配算法。在平台-目标分配算法中所需的攻击优势指数的计算上,提出利用SVDDBNs进行攻击优势指数的计算。由于SVDDBNs具有可以融合不同类型信息进行推理决策的特点,因此给出的目标分配算法考虑的因素更加全面,计算结果具有更高的置信度。最后的仿真算例证明了此方法的正确性和有效性。     

声自导鱼雷一次转角射击参数的优化

为了提高声自导鱼雷一次转角射击的发现概率,建立了一次转角射击的解析模型,并将射击参数的优化归结为一个带约束的优化问题。使用了一种改进的粒子群算法解决了上述问题,优化了自导扇面相遇点系数和出管直航距离两个射击参数。实验结果表明,使用优化后的射击参数显著提高了鱼雷的发现概率。     

等效模拟压制下雷达探测区域计算与调整

压制干扰下的雷达探测区域能够形象反映雷达在压制干扰下的作战能力。理论计算出的雷达探测区域可能与实际情况相差很大,为了获得较为精确的探测区域,提出通过等效模拟压制干扰下的外场飞行试验获得雷达探测区域调整因子,并依据调整因子对理论探测区域进行调整。通过数字仿真初步验证了等效模拟压制技术的可行性,并通过数字仿真飞行试验初步验证了雷达探测区域调整方法的可行性,为日后依据外场飞行试验调整雷达探测区域提供支持。     

一种探雷声纳图像分割方法及应用

提出一种适用于探雷声纳图像的疑似水雷目标扫描分割方法。该方法以图像区域生长法为基础,根据探雷声纳的成像原理及水雷目标的图像特性,对区域生长法中的参数做了特别设定,分搜索和定位两步对图像中疑似目标进行扫描分割,讨论了搜索和定位两种扫描窗口的尺寸及扫描方法。将该方法应用于实际探雷声纳图像,可得到符合预定信混比要求的疑似目标区域,为基于探雷声纳图像的水雷自动判别奠定了基础。     

挠性航天器变幅值输入成形姿态机动策略

针对变参数挠性航天器的姿态机动问题,在变幅值零振动成形器的基础上,提出了鲁棒性较强的变幅值零振动和零微分成形器设计方法,设计了鲁棒姿态机动策略.该机动策略的控制目标是,将航天器机动到期望状态的同时,消除挠性结构的残余振动.以含转动挠性太阳翼的航天器进行三轴姿态机动为例,进行数值仿真.仿真结果表明,该机动策略对挠性结构频...     

Cooperative interception with fast multiple model adaptive estimation

For the case that two pursuers intercept an evasive target, the cooperative strategies and state estimation methods taken by pursuers can seriously affect the guidance accuracy for the target, which performs a bang For the case that two pursuers intercept an evasive target, the cooperative strategies and state estimation methods taken by pursuers can seriously affect the guidance accuracy for the target, which performs a bang-bang evasive maneuver with a random switching time. Combined Fast multiple model adaptive estimation (Fast MMAE) algorithm, the cooperative guidance law takes detection configuration affecting the accuracy of interception into consideration. Introduced the detection error model related to the line-of-sight (LOS) separation angle of two interceptors, an optimal cooperative guidance law solving the optimization problem is designed to modulate the LOS separation angle to reduce the estimation error and improve the interception performance. Due to the uncertainty of the target bang-bang maneuver switching time and the effective fitting of its multi-modal motion, Fast MMAE is introduced to identify its maneuver switching time and estimate the acceleration of the target to track and intercept the target accurately. The designed cooperative optimal guidance law with Fast MMAE has better estimation ability and interception performance than the traditional guidance law and estimation method via Monte Carlo simulation.