Multidisciplinary design modeling and optimizationfor satellite with maneuver capability

According to the mission of a satellite with maneuver capability, the collaborative optimization (CO) method was introduced for the satellite system design, and the related multidisciplinary design optimization (MDO) model was established. The possessing and needed velocity increments Δv and Δv _{n e e d} were taken as the measurement of maneuvering capability of the studied satellite, which were then combined with total mass of the satellite to form the optimization objective in the systematic level of the MDO problem. The design variables and constraints of the MDO problem dealt with disciplines or subsystems as guidance, navigation and control (GNC), power, and structure, and corresponding engineering analysis models were also built. A program system to solve the MDO problem wasdeveloped by integrating a non-nested CO method, the commercial and user-supplied codes on framework software iSIGHT. The result showed that the satellite performance could be obviously improved, which also indicates MDO technique is feasible and effective for the spacecraft design problem. The modeling and optimization procedure of the work can be referred for further research and engineering design.     

Dynamic surface control of a piezoelectric fuel injector during rate shaping

Fuel injection rate shaping is a strategy to improve fuel efficiency and reduce harmful emissions in diesel engines. Due to their fast response, piezoelectric fuel injectors are capable of rate shaping operation. This paper describes a model-based closed-loop controller of injection flow rate for a piezoelectric fuel injector. This within-an-engine-cycle control strategy utilizes a dynamic surface control scheme and shows an injection flow rate tracking capability. Practical issues with LabVIEW FPGA control implementation are also addressed. The performance of the controller is verified with simulation and experimental results at different rail pressures and desired injection rates. The experiments show a maximum error of total fuel per one injection event of 2.5%. A stability analysis is also included.     

基于傅里叶级数的小推力航天器快速轨迹设计

为了满足小推力航天器交会轨迹的快速性设计需求,基于形状逼近理论,设计了一种三维轨迹模型.将轨迹设计问题转换为求解傅里叶级数的系数问题,避免了轨迹运动方程非线性强、难以求解的难题,极大地提高了计算效率.考虑到推力加速度的限制,建立了加速度约束方程,并结合轨迹的运动方程,给出了傅里叶级数的求解过程.同时根据边界条件和最大推力加速度值,定性地分析了傅里叶系数的存在条件.仿真验证了该方法的正确性和可行性,并从计算效率上与高斯伪谱法进行了对比,结果表明本文的方法计算耗时仅为高斯伪谱法的0.67%.     

异氰酸酯增强二氧化硅气凝胶的力学性能

采用有机无机复合的方式,制得异氰酸酯增强的SiO2气凝胶。将硅酸甲酯(TMOS)、甲基三甲氧基硅烷(MTMS)、3-氨丙基三乙氧基硅烷(APTES)配成混合硅源,经水解缩聚后形成凝胶,老化后浸泡在含六亚甲基二异氰酸酯单体(HDI)的乙腈溶液中,最后经CO₂超临界干燥,获得了具有良好机械性能的SiO₂气凝胶。制备过程中引入的MTMS增加了凝胶与有机物间的浸润性,与使用有机物低聚体相比,使用单体可使有机物更易进入凝胶网络,反应更充分,形成纳米尺度更均匀的复合气凝胶。复合后的气凝胶密度为330 mg/cm³、比表面积为446.3 m²/g、热导率为0.068 W•m^-1•K^-1,该气凝胶良好的力学性能(压缩强度为19.96 MPa、压缩模量为82.37 MPa)使气凝胶的机械加工成为可能。     

Elastic impact of spheres on thin shallow spherical shells

This investigation was concerned with the elastic impact of spheres on thin shallow spherical shells. A non-linear integro-differential equation of the impact process was developed on the basis of Reissner's approximate theory for transverse vibrations of shallow shells and the quasistatic Hertzian impact theory. This equation was numerically integrated and its main results were experimentally verified. Special attention was given to the apparently new observations that the rebound height of a sphere dropped onto a given shell has a minimum value for a critical size of the sphere, and that the contact time differs substantially for sphere sizes greater or less than this critical value.     

低信噪比下基于YOLOv3的昆虫目标检测

掌握昆虫迁飞规律对于农业防治和生态学研究具有重大意义,雷达正是检测昆虫迁飞最有效的手段.昆虫回波弱,传统的恒虚警检测(Constant False Alarm Rate,CFAR)算法在低信噪比(Signal To Noise Ratio,SNR)时的检测性能下降;同时昆虫目标体积小、飞行速度慢,在距离维和多普勒维的扩...     

基于全相位FFT的稳健型时间调制阵列测向

基于谐波特征分析的时间调制阵列测向方法的正确性与精度严重依赖接收谐波的估计精度. 传统的离散傅里叶变换(discrete Fourier transform, DFT)或快速傅里叶变换(fast Fourier transform, FFT)在估计谐波的幅相时,由于信号频率通常偏离采样频率的整数倍,会形成栅栏效应,从而引起基于谐波特征分析的时间调制阵列测向的精度降低甚至失效. 针对该问题,本文将全相位FFT引入二单元时间调制阵列接收谐波的分析中,通过提升谐波幅相估计的鲁棒性来提升时间调制阵列测向方法的稳健性. 仿真结果表明,当信号的载频为频谱分辨率的任意小数倍时,提出的全相位FFT时间调制阵列测向方法均能正确测向,且随着信噪比的增加,测向均方根误差收敛至0. 本文工作提升了基于谐波特征分析的单通道时间调制阵列测向方法的稳定性。     

星载SAR方位模糊研究

本文根据方位模糊产生机理详细分析了方位向成像处理参数、波长、方位方向图副瓣对方位模糊的影响.通过分析可知:方位分辨率相同时,低频段SAR系统模糊问题更严重,但可通过提高重频、压低方向图副瓣电平等方法可改善方位模糊,最后仿真验证了上述结论并给出改善方位模糊的设计考虑.     

自适应机翼的发展现状及其关键技术研究

综述了近二十年来国内外自适应机翼技术的研究现状以及该领域需要解决的关键技术,对未来这一技术的发展和应用进行了展望。     

Three-dimensional viscous flow and heat transfer over a permeable shrinking sheet

This paper presents a numerical analysis of a steady three-dimensional fluid flow and heat transfer towards a permeable shrinking sheet. The governing nonlinear partial differential equations are transformed into a system of ordinary differential equations by a similarity transformation, which are then solved numerically by a shooting method. The effects of the governing parameters on the skin friction and heat transfer from the surface of the shrinking surface are illustrated graphically. It is found that dual solutions exist for the shrinking case. A comparison with known results from the open literature has been done and it is shown to be in excellent agreement.