实现非定常耦合流动对轴流压气机叶片动力响应问题的探讨

本文针对“在轴流压气机中实现非定常耦合流动状态时,是否会引发下游转子产生结构振动问题”进行了研究。在已有的三维非定常CFD计算频谱分析结果的基础上,使用有限元方法进行模态分析,通过调整上游静叶数的手段,研究实现耦合流动后产生的动力响应问题,并对调整前后压气机的气动特性进行比较。结果证明,通过适当的调整上游静子叶片数,可以在最大化发掘非定常耦合流动的潜力的同时避开转子的共振频率。     

Multi-objective optimal formation reconfiguration with scalarization and stochastic boundaries

A new method is proposed for multi-objective optimal control of satellite formation reconfiguration. First, necessary optimality conditions of single-objective fuel-optimal reconfiguration are studied. Problem of initial guess of the costate and control discontinuity are addressed by using a new developed stochastic based method. Terminal conditions of Two Point Boundary Value Problem (TPBVP) of the optimal control equations are relaxed using augmented Gaussian. Variances or bandwidths of the terminal conditions are set to decision variables to be optimized. Responses of varied initial costate are modeled and propagated using Riccati equation. Using quadratic convolution of relaxed terminal conditions, objective function of the fuel-optimal problem is reformulated into a quadratic equation, and a gradient based optimizer is used to search the optimal initial guess. In the second part of the paper, optimal control of format flying reconfiguration with two competitive objectives:fuel and time of flight (ToF) is studied. With Pascoletti-Serafini scalarization, the Multi-objective Optimal Control Problem (MOCP) is scalarized into a set of weighted Single-objective Optimal Control Problems (SOCP). Hamiltonian and switch function for the weighted SOCP are developed and constructed. New developed stochastic based approach is then used to search the optimal Pareto solutions. Verification and performances of proposed algorithms are demonstrated through numerical simulations of single-objective and multi-objective optimal control of low-thrust elliptical orbit formation reconfiguration. Potential applications of the algorithms to some other preliminary space mission designs are also discussed.     

Long-term time-varying characteristics of UPD products generated by a global and regional network and their interoperable application in PPP

The quality and availability of Uncalibrated Phase Delay (UPD) solutions are crucial to the Precise Point Positioning (PPP) service, and the long-term temporal variability and its contributing factors should be better understood. In this paper, we comprehensively investigate the long-term time-varying characteristics of each UPD product respectively generated by a global and regional network and their interoperable application in PPP-AR (ambiguity resolution), the sampling of the WL and NL UPDs are daily and 30 s, respectively. Firstly, in terms of our 30 day Wide-Lane (WL) UPD products of 31 satellites, the Standard Deviation (STD) of each satellite WL UPDs ranges from 0.04 to 0.06 cycles, indicating that the long-term prediction accuracy of satellite WL UPD is sufficient for fixing Wide-Lane ambiguities. Secondly, when a satellite in eclipsing the discontinulity may corrupt the determination of Narrow-Lane (NL) UPD in form of offset, as a result of lacking or poor satellite attitude dynamic modeling. When the influence of discontinuity is removed, the STD of our estimated satellite NL UPDs is less than 0.05 cycles. Thirdly, the STD of our estimated receiver WL UPDs is mainly below 0.2 cycles, which implies that its stability is one order poorer that of the satellite. In addition, if they are used for stations in and around the network covered region, the stability of the UPD products from the CMONOC (Crustal Movement Observation Network of China) is better than that from a global network, benefit from the fact that all the CMONOC stations are equipped with the same receiver type. Finally, the PPP-AR results show that a rate of 82.9% for stations with a WL-ambiguity-fixed rate of over 90% while 69.5% for stations with an NL-ambiguity-fixed rate of over 80% can be achieved when using UPD from the global network, which is worse than that of using UPD from the CMONOC (85.7% for stations with a WL-ambiguity-fixed rate of over 90% while 75% for stations with an NL-ambiguity-fixed rate of over 80%). The results of the experiment on the UPD interoperable application in PPP show that the global network UPD products can provide a fast AR at any single station, and the convergence time is well below 25 min. Particularly, when the location of a station is in and around the regional network, our results show that the PPP results obtained using regional UPDs enable the consistent use of global UPDs. When the location of a station is far away from the regional network, using the regional UPDs can not achieve PPP-AR. Finally, the WL UPDs of the previous day is used for forecasting to estimate the NL UPDs, the stability analysis results of NL UPDs solution and positioning results are demonstrate the validity of forecasted UPD products.     

法向发身率测量仪

本文给出了在大气温度下测量物质表面法向发射率的原理、装置结构及测试结果。这个装置是由黑体,样品腔和辐射计(接收元件)构成。法向发射率是由在相同温度下样品产生的热电势EMF与黑体产生的热电势EMFo之比来度量的。最后,对误差进行了讨论。     

含间隙球轴承-转子系统的主共振研究

 为了深刻揭示球轴承-转子系统的共振机理,考虑了重力、装配等因素引起的非对称轴承间隙以及滚珠与滚道之间的Hertz接触,建立了球轴承-转子系统的运动方程,首次应用平均法求得了系统在主共振情况下的解析解,并讨论了系统参数对主共振的影响。根据奇异性理论方法计算得到了系统参数平面上的转迁集,研究了不同参数域内共振解的分岔模式,最后通过数值仿真验证了理论分析的正确性,从而为球轴承-转子系统的振动控制提供了理论依据。     

分区多重网格法在复杂区域中的数值研究

突破多重网格方法在多连通域中应用的局限性,将分区法与多重网格法结合,形成分区多重网格法,应用在复杂几何域及复杂多连通域中,结果表明,它不仅能提高精度,而且能加快收敛。     

末制导导引头定位精度的雷达误差分析

研究复合制导的战术导弹中末制导交班的导引头预定精度问题.提出用小扰动法分析导引头预定参数对误差源的误差敏感性关系.以中远程防空导弹为例,结合导弹运动方程组和目标运动模型,计算了中末制导交班的导引头预定参数,并计算了在制导站雷达测量误差下的末制导导引头预定参数的计算精度.可知,导引头定位参数的计算误差随着弹目距离的接近而显著增大,得到中末制导交班不能太晚的重要结论.     

可实现定点停泊与轨迹逼近的航天器交会控制

许多空间任务均需进行轨道交会,据任务的不同,对轨道交会的要求也不同,某些情况下需要跟踪星在交会的过程中暂时停泊于某一点,某些情况下对交会过程的视线角与轨迹提出一定的要求.针对这种需求,设计了一种闭环反馈控制方法,可以使跟踪星在设定的某点进行停泊及停泊保持,也可以沿设定的某条轨迹逼近目标,以满足不同任务对交会过程的不同要求.经仿真表明,此方法能够很好的满足任务要求,并具有精度高、能耗低、跟踪速度快的特点.     

坐标测量机上平面度误差的快速评定

把测点到基准平面的轴向距离作为度量函数来建立平面度误差评定的线性模型，从而快速地评定出空间一般位置被测平面的平面度误差，为坐标测量机采用最小条件准则评定平面度误差提供了一个实用方法。