载波相位平滑伪距算法在区域实时定位系统中的应用

针对可能出现的伪距突发错误及载波周跳的问题,研究一种应用于低动态区域实时定位系统的鲁棒载波相位平滑伪距算法.仿真结果表明,方法可以在一定程度上减小由于伪距突发错误与周跳所引起的测距误差,进而提高定位精度.     

Attitude tracking control for variable structure near space vehicles based on switched nonlinear systems

An adaptive robust attitude tracking control law based on switched nonlinear systems is presented for a variable structure near space vehicle (VSNSV) in the presence of uncertainties and disturbances. The adaptive fuzzy systems are employed for approximating unknown functions in the flight dynamic model and their parameters are updated online. To improve the flight robust performance, robust controllers with adaptive gains are designed to compensate for the approximation errors and thus they have less design conservation. Moreover, a systematic procedure is developed for the synthesis of adaptive fuzzy dynamic surface control (DSC) approach. According to the common Lyapunov function theory, it is proved that all signals of the closed-loop system are uniformly ultimately bounded by the continuous controller. The simulation results demonstrate the effectiveness and robustness of the proposed control scheme.     

A new simpler rotation/curvature correction method for Spalart-Allmaras turbulence model

 A new and much simpler rotation and curvature effects factor, which takes the form of Richardson number suggested by Hellsten originally for SST k-x model, is presented for Spalart and Shur's rotation and curvature correction in the context of Spalart-Allmaras (SA) turbulence model. The new factor excludes the Lagrangian derivative of the strain rate tensor that exists in the SARC model, resulting in a simple, efficient and easy-to-implement approach for SA turbulence model (denoted as SARCM) to account for the effects of system rotation and curvature, techniquely. And then the SARCM is tested through turbulent curved wall flows: one is the flow over a zeropressure- gradient curved wall and the other is the channel flow in a duct with a U-turn. Predictions of the SARCM model are compared with experimental data and with the results obtained using original SA and SARC models. The numerical results show that SARCM can predict the rotation-curvature effects as accurately as SARC, but considerably more efficiently. Additionally, the accuracy of SARCM might strongly depend on the rotation-curvature model constants. Suggesting values for those constants are given, after some trials and errors.     

一种宽频被动雷达制导信号的鲁棒滤波方法

探索提高制导武器末制导系统抗噪声扰动鲁棒性的技术方法,研究了一种能将制导信号不确定噪声引起的滤波估计误差控制在一定边界范围内的鲁棒滤波算法,采用该算法对宽频被动雷达导引头测量输出信息滤波估计,可以弱化不确定随机噪声对制导系统的扰动,从而提高制导系统抗噪声扰动的鲁棒性.通过仿真验证了算法的有效性.     

A satellite schedulability prediction algorithm for EO SPS

With notably few exceptions, the existing satellite mission operations cannot provide the ability of schedulability prediction, including the latest satellite planning service (SPS) standard-Sensor Planning Service Interface Standard 2.0 Earth Observation Satellite Tasking Extension (EO SPS) approved by Open Geospatial Consortium (OGC). The requestor can do nothing but waiting for the results of time consuming batch scheduling. It is often too late to adjust the request when receiving scheduling failures. A supervised learning algorithm based on robust decision tree and bagging support vector machine (Bagging SVM) is proposed to solve the problem above. The Bagging SVM is applied to improve the accuracy of classification and robust decision tree is utilized to reduce the error mean and error variation. The simulations and analysis show that a prediction action can be accomplished in near real-time with high accuracy. This means the decision makers can maximize the probability of successful scheduling through changing request parameters or take action to accommodate the scheduling failures in time.     

随机应力下系统可靠度的鲁棒优化

在随机应力条件下建立加速退化模型,设计加速退化试验并估计模型参数,用数学近似方法推导了可靠性均值和方差的计算模型,分别作为鲁棒优化设计模型的约束与目标函数。燃烧室可靠性设计算例结果表明:该方法不仅使系统设计达到可靠性要求,而且有较高的稳健性,有一定的工程实际意义。     

Robust decentralized control design for aircraft engines: A fractional type

A new decentralized control for aircraft engines is proposed. In the proposed control approach, aircraft engines are considered as uncertain large-scale systems composed of interconnected uncertain subsystems. For each subsystem, the time-varying uncertainty, including parameter disturbances and interconnections in/between subsystems, is depicted by a class of general nonlinear functions. A fractional robust decentralized control with two parts, the nominal one and the fractional one, is presented. The nominal control guarantees the asymptotical stability of the engine system without uncertainty. The fractional part aims at overcoming the influences of uncertainty. Compared to the previous studies, the presented control provides not only an extra flexibility for the system performance tuning by the fraction-type gain but also a facility for the control input calculation. The proposed control approach is applied to a turbofan engine with two subsystems. The computer simulation shows that, in the flight envelope, the fractional control not only guarantees the closed-loop system uniform boundedness and ultimate uniform boundedness but also shows good economy.     

RSSI测距在蓝牙室内定位抗差算法中的应用

蓝牙信号强度在室内环境下易受人员扰动等环境因素影响,从而影响定位精度。基于RSSI测距的蓝牙室内定位原理,将人员等扰动视为异常误差,采用胡贝尔、汉佩尔、IGG和LEGE四种抗差算法,比较分析了不同抗差算法的定位提升效果。试验结果表明,不管有无人员扰动,四种抗差算法均可改善定位精度,其中IGG法定位精度最高,约为3m,且有较好的稳定性。     

减少飞机对风切变敏感性的研究

本文用时域内改变加权阵Q方法,优化设计有风切变时飞机的下滑控制系统。在设计过程中将风切变强度v′_f作为系统中的一个变量,使设计出的系统对风切变强度的灵敏度减少,即系统具有鲁棒稳定性。为了比较,文中还用二次型性能指标优化设计同一个系统。另外对性能指标中加权阵Q和鲁棒矢量加权阵Q_5元素的选取作了探索。