Design and Simulation of TF and TA Controller for Missile

A nonlinear terrain following(TF) and terrain avoidance(TA) controller is proposed for missile control systems. Based on classical TF algorithm (adaptive angle method), a new method for TF controller is proposed by using angle of attack. A method of obtaining terrain outline data from digital elevation map (DEM) for TF control is discussed in order to save store space. A TA algorithm is proposed by using bank-to-turn technique. The block control model, which is suitable for backstepping design, is given for nonlinear model of missile. Making full use of the characteristics of the system and combining block control principle and backstepping technique, a robust controller design method is proposed. Uncertainties in every sub-block are allowed, and can be canceled by using the idea of nonlinear damping. It is proved that the state tracking errors are converged to a neighborhood of the origin exponentially. Finally, nonlinear six-degree-of-freedom simulation results for the missile model are presented to demonstrate the effectiveness of the proposed control law.     

基于高斯过程回归的空天飞行器多精度气动建模方法

为了满足空天飞行器在初步设计阶段宽速域、大空域模型的需求,将传统工程估算方法和计算流体动力学（CFD）数值模拟方法分别作为低精度和高精度气动数据来源,基于高斯过程回归模型提出独立于构型的空天飞行器气动性能多精度气动建模方法.在工程估算方法中,以面元法为基础,建立空天飞行器气动力快速估算模型.在CFD数值模拟中通过求解三维可压缩Euler方程实现空天飞行器气动高精度计算.将所提出的多精度气动建模方法应用于FTB外形的双参数气动建模问题中,通过对比分析,发现所提出的多精度气动模型的预测精度、稳定性均优于用同等数量高精度样本构建的单精度代理模型的,预测的相对误差小于1%.将多精度气动模型作为该空天飞行器再入问题气动数据来源,对比分析单、多精度建模方法对再入轨迹仿真的影响,发现所提出的空天飞行器多精度气动建模方法能够更加快速、准确地给出轨迹仿真所需的气动数据.     

浅谈如何保养羊毛衫

羊毛是纺织工业的重要原料．具有许多优良特性．如弹性好、吸湿性强、保暖性好、不易沾污、光泽柔和等。在冬季里,羊毛产品受到广大消费者的青睐．虽然羊毛的纺织品价格昂贵,但人们依然对它“情有独钟”。