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181.
The development of a powerful parameter estimation routine and its integration into the simulation environment HOST is described. With this tool approaches are being made towards new strategies of mathematical modeling, aimed at providing highly accurate and nevertheless run-time efficient simulation models. The identification routine is capable of optimizing parameterized models in both dynamic time domain simulation and static (e.g. trim state variation) conditions. Examples of both cases are presented to emphasize the improvement in the system response prediction and to demonstrate the abilities of the identification techniques in combination with the nonlinear simulation platform. This article reviews the activities and achievements accomplished by the DLR Institute of Flight Research and the ONERA Systems Control and Flight Dynamics Department during the last few years in the research on rotorcraft flight dynamics modeling and model identification. Future activities that require extensive high fidelity modeling are in the scope of the current and coming modeling activities that include the use of the presented methods and software technologies.  相似文献   
182.
Bistatic SAR (BSAR) systems have recently been the subject of several studies, but little attention has been given to the potential of the location of targets. In the paper, the performance of the estimation of 3-D position of a target (TPE) in parasitic SAR is obtained analytically and illustrated by computer simulation using ambiguity function analysis, and the maximum likelihood estimate (MLE) approach. It was shown that by using a multi look parasitic BSAR all three coordinates of an isolated point target (IPT) could be evaluated. Analytical closed form equations that characterize the measurement accuracy were derived. In the final these equations will be used to demonstrate various cases of more practical, including optimal trajectories choice under any geometry configuration case, moreover, the conclusion is verified via Matlab.  相似文献   
183.
重点研究挠性空间结构的H∞辨识,研究表明:依据系统的输入输出空间,对系统的未知动力学参数估计和对高维数截断的适当操作,将导致适合于控制的低维数学模型。模型维数确定时,系统模型与实际系统的距离在H∞范数的意义下几乎为最小,模型维数足够大时,系统模型与实际系统的距离可任意小,这是文下间提出了挠性空间结构H∞辨识的基本思想,为此,以带挠性梁的卫星系统为背景,首先分析了系统的动力学特性,引入了挠性系统H∞  相似文献   
184.
介绍了寿命周期费用的概念以及各阶段分布情况;针对经典回归分析的不足,采用偏最小二乘回归分析对某装备样本数据进行分析建模;建立了研制费用与几个相关指标的回归方程,并将估算结果与经典的回归分析进行对比,验证模型的合理性。该模型能较好地反映了费用与各指标之间的关系,对后续寿命周期费用的分析与控制有一定的意义。  相似文献   
185.
确定无陀螺卫星姿态的二阶非线性滤波算法研究   总被引:1,自引:0,他引:1  
应用基于二阶泰勒级数近似得到的非线性滤波技术,设计了利用星敏感器矢量观测信息确定无陀螺三轴稳定卫星姿态的二阶非线性滤波算法.结合矢量观测的特点,分别讨论了单矢量观测信息与多矢量观测信息的处理方法,并把QUEST算法作为矢量观测数据压缩技术有效地结合进姿态估计器中,使得多矢量观测情况下的滤波修正算法得到了简化.仿真测试结果证明,二阶非线性姿态估计器的滤波性能要优于传统的扩展卡尔曼滤波姿态估计算法.  相似文献   
186.
Angle of Attack(AOA) is a crucial parameter which directly affects the aerodynamic forces of an aircraft.The measurement of AOA is required to ensure a safe flight within its designed flight envelop.This paper intends to summarise a comprehensive survey on the measurement techniques and estimation methods for AOA, specifically in Unmanned Aerial Vehicle(UAV) applications.In the case of UAVs, weight constraint plays a major role as far as sensor suites are concerned.This results in selecting a su...  相似文献   
187.
In this paper, we present a distributed framework for the lidar-based relative state estimator which achieves highly accurate, real-time trajectory estimation of multiple Unmanned Aerial Vehicles(UAVs) in GPS-denied environments. The system builds atop a factor graph, and only onboard sensors and computing power are utilized. Benefiting from the keyframe strategy, each UAV performs relative state estimation individually and broadcasts very partial information without exchanging raw data. The com...  相似文献   
188.
Ballistic Missile Trajectory Prediction(BMTP) is critical to air defense systems. Most Trajectory Prediction(TP) methods focus on the coast and reentry phases, in which the Ballistic Missile(BM) trajectories are modeled as ellipses or the state components are propagated by the dynamic integral equations on time scales. In contrast, the boost-phase TP is more challenging because there are many unknown forces acting on the BM in this phase. To tackle this difficult problem, a novel BMTP method by ...  相似文献   
189.
This study uses the Neural Network(NN) technique to optimize design of surfacemounted Permanent Magnet Synchronous Motors(PMSMs) for More-Electric Aircraft(MEA)applications. The key role of NN is to provide dedicated correction factors for the analytical PMSM mass and loss estimation within the entire design space. Based on that, a globally optimal design can be quickly obtained. Matching the analytical estimation with Finite-Element Analysis(FEA) is the main research target of training the NN. ...  相似文献   
190.
《中国航空学报》2022,35(12):1-31
The transmit antenna beampattern of the phased array radar is only a function of angle, limiting its ability to discriminate the targets from the same direction. Recently, the waveform diverse array radars expand the angle-dependent beampattern to an angle-time-range-dependent three-dimensional function by modulating the frequencies/time delays/phases across different transmit antenna elements. In this respect, extra Degrees-of-Freedom (DOFs) in the range domain are achieved, which opens up an innovative way to fulfil the tasks with enhanced system performance by jointly using the angle and range information. This paper summaries the developments of waveform diverse radars, including the Frequency Diverse Array (FDA), the Space-Time-Circulating-Array (STCA), and the Element-Pulse-Coding (EPC) frameworks, with emphasis on the analysis of the range-dependent beampattern from the basic properties upon how it is controlled. Moreover, the most recent advances of utilizing such a range-dependent beampattern in target detection, parameter estimation and identifiability, clutter suppression, jammer suppression and Synthetic Aperture Radar (SAR) imaging are discussed.  相似文献   
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