A robust semi-analytic method to solve the minimum ΔV two-impulse rendezvous problem

A novel semi-analytic approach is developed to determine the minimum $\mathrm{\Delta }V$ for a two-impulse rendezvous and validated both empirically and analytically. A previously published closed-form $\mathrm{\Delta }V$ estimate and the Lambert minimum energy transfer is used to establish upper and lower bounds of the minimum $\mathrm{\Delta }V$ transfer between two orbits. These bounds, in conjunction with the bisection method, operate on a nonlinear radical cost function to guarantee linear convergence. This approach has several real world applications including a low earth orbit (LEO) to highly elliptical orbit (HEO), and a HEO to retrograde geosynchronous orbit transfer. The minimum $\mathrm{\Delta }V$ estimates are better than those reported in the existing literature, while run times improved as much as two orders of magnitude over a fixed time Lambert solver. All singularity cases were addressed such that any orbital geometry, including Hohmann and radial elliptic transfers, converged to the global minimum $\mathrm{\Delta }V$. This approach will work for both coplanar and non-coplanar 3D geometries for any orbit type.     

燃气源控制气流非稳态耦合传热问题研究(Ⅰ)--计算模型和方法

针对某燃气源控制气流与导热套环之间的非稳态耦合传热问题,建立了数学模型,并采用整体求解的方法进行求解,即把流体区域的流动和对流换热与固体区域的导热过程组合起来,作为一个统一换热过程来处理。为确保计算结果在物理上的真实性,采用“假密度”法求解以温度T为求解变量的能量方程。对于非稳态控制方程离散后的离散方程采用了PISO方法进行求解。     

超（近）临界压力航空煤油RP-3的拟过冷沸腾传热特性

为了研究吸热型碳氢燃料在新型飞行器中的再生冷却性能,采用电加热方式,在热流密度0.1-1.0MW/m2和质量流速500-1000kg/m2s条件下,小通道圆管内（D=1.6mm）研究了超（近）临界压力下（P=3MPa）航空煤油RP-3的拟沸腾流动传热特性。研究发现了超（近）临界压力航空煤油的拟过冷沸腾传热现象。拟过冷沸腾壁温变化特征和传热恶化特征与亚临界压力下的相应特征存在差异。超临界压力航空煤油传热区域划分为类液态强制对流传热区、拟过冷沸腾区和类气态强制对流传热区。拟过冷沸腾壁温和传热系数随流体温度增加而缓慢增加,起到传热强化的作用;拟临界温度区域,存在传热系数极小值点,燃料发生传热弱化;燃料温度大于拟临界温度,燃料处于超临界类气态,传热大幅强化。     

SPMSM弱磁算法自适应调速仿真

摘要： 为提高弹用电动舵系统轻负载情况下的最大舵偏角速度,并抑制负载扰动,在表贴式永磁同步电机空间矢量控制算法的基础上提出弱磁自适应控制策略.采用基于电机物理功率限制的弱磁控制算法,实现调速系统在轻负载功率富余时的弱磁升速.设计基于Lyapunov稳定性的速度自适应控制器,克服速度环采用传统PI调节算法时随着负载变化时动态性能弱的缺点. 通过Simulink仿真证明该算法能够在实现弱磁升速的同时,具备良好的负载扰动抑制性能.     

感应电动机磁链观测与参数在线辨识方法研究

针对感应电动机在矢量控制过程中存在的转子磁链定向不准确的问题,解释了磁链观测误差的原因,重点研究了电机参数的在线辨识方法。提出了基于模型参考自适应系统的感应电动机磁链观测与参数在线辨识方法。基于波波夫超稳定性定理,设计了转子时间常数与励磁互感的双参数自适应律。该方法以电压模型磁链观测器作为参考模型,在线辨识出电流模型磁链观测器所需的参数,使磁链观测结果具有收敛性和鲁棒性,从而避免了电机参数测量不准确与容易变化对磁链定向造成的不良影响。仿真结果表明该方法具有实时性与可行性。     

旋转盘腔稳态换热试验的时间相关性

在稳态换热试验中,试验没有达到稳定就测量会增大误差,常见工况中盘面平均努塞尔数Nu误差的半衰期为2500~2700s。为判断试验是否达到稳定或可测量状态,采用瞬态计算方法对旋转盘腔换热试验的稳定时间的判定方法进行了研究。数值计算结果表明:对于旋转盘腔换热试验,稳定时间较长。提供了一种通过试验精度判定稳定时间和可测时间的方法,试验前可以由固体非稳态导热的傅里叶数估算可测时间。建议试验过程中每隔一段时间观测传感器数值,观测时间间隔按对数规律确定,直到传感器数值不变以确定达到稳定状态。      

Experimental study on film cooling performance of imperfect holes

An experimental study is made to investigate the film cooling performance of imperfect holes due to in-hole blockage over a flat plate. A specifically pyramid-shaped element is used to simulate the in-hole blockage. Six in-hole blockage orientations (such as leading-inlet, leading-middle, leading-exit, trailing-inlet, trailing-middle and trailing-exit) and four blocking ratios (ranging from 0.1 to 0.4) are taken into considerations. Based on the experimental results, the influences of in-hole blockage on the film cooling effectiveness and discharge coefficient under typical blowing ratios are analyzed. It is confirmed that the in-hole blockage results in a reduction of discharge coefficient related to the perfect film cooling holes, especially for the leading-exit and trailing-inlet orientations with a big blocking ratio. However, in the view of film cooling effectiveness, the in-hole blockage shows complicated affecting roles. In general, except for the leading-exit orientation, the in-hole blockages produce detrimental influence on the film cooling effectiveness.     

带有冗余度的新型连续地月载荷转移系统动力学与能量分析

传统的连续地月载荷转移系统(CCPTS）存在可靠性低、转移效率差的问题。设计了带有冗余度的新型连续地月载荷转移系统(N-CCPTS）,其带有的一套冗余抓捕机构不但提高了系统的可靠性,而且可以运载载荷,将转移效率提高了1倍。计算和仿真结果表明,冗余机构对系统参数变化规律的影响是小量;在转移相同质量的载荷时,当椭圆轨道远地点的半径足够大时,N-CCPTS相比CCPTS更加节省能量。N-CCPTS可以为高效率的连续地月物资转移提供一种更加可行的方案。     

基于改进型MRAS无轴承异步电机矢量控制系统转速辨识研究

以改进电压模型转子磁链为基础,构建了无轴承异步电机转子磁链定向无速度传感器矢量控制系统。MATLAB/Simulink仿真结果表明:与传统方法相比,所提出的改进电压模型转子磁链提高了转子磁链的观测精度;同时,基于无轴承异步电机转子磁链定向无速度传感器矢量控制系统,在空载调速和加载情况下,辨识转速和实测转速具有很好的一致性,电机能够稳定悬浮运行,充分验证了所提方案的有效性。