GPSNISNAV integrated relative navigation and attitude determination system for ultra-close spacecraft formation flying

For the improvement of accuracy and better fault-tolerant performance, a global position system (GPS)/vision navigation (VISNAV) integrated relative navigation and attitude determination approach is presented for ultra-close spacecraft formation flying. Onboard GPS and VISNAV system are adopted and a federal Kalman filter architecture is used for the total navigation system design. Simulation results indicate that the integrated system can provide a total improvement of relative navigation and attitude estimation performance in accuracy and fault-tolerance.     

一种新型UUV半实物仿真系统设计与实现

针对UUV导航与控制系统高精度仿真的需要,设计了一种支持捷联惯导、多普勒测速仪、深度传感器和GPS接收机接入的半实物仿真系统,解决了GPS卫星导航信号仿真、多普勒测速仪水声回波模拟和UUV深浅水航行深度模拟问题,进行了导航与控制系统的半实物仿真试验,分别测试了GPS导航仿真子系统、多普勒测速仿真子系统和深度模拟子系统。试验结果表明,该仿真系统满足了仿真实时性和计算精度的要求,对于UUV研制具有重要的应用价值。

Abstract：

To satisfy the requirement of high accuracy simulation of complicated navigation and control system of unmanned underwater vehicle, a new plan of simulation system was proposed, which afforded the interface environment for SINS, Doppler velocity instrument, depth sensor and GPS receiver. The GPS satellite navigation signal simulation, the acoustic echo of Doppler velocity instrument and the sailing depth simulation were solved. The simulation experimentation combining hardware was processed, and the GPS simulation subsystem, the Doppler velocity simulation subsystem and the sailing depth simulation subsystem were all tested. The results show that the simulation system meets the real-time and accuracy requirements, and the system has important application value for UUV development.     

Research on robust fault-tolerant control for networked control system with packet dropout

A kind of networked control system with network-induced delay and packet dropout, modeled on asynchronous dynamical systems was tested, and the integrity design of the networked control system with sensors failures and actuators failures was analyzed using hybrid systems technique based on the robust fault-tolerant control theory. The parametric expression of controller is given based on the feasible solution of linear matrix inequality. The simulation results are provided on the basis of detailed theoretical analysis, which further demonstrate the validity of the proposed schema.     

Stability Analysis and Performance Evaluation of Delayed Bilateral Telerobotic Systems over a Lossy Communication Channel

The focus of this paper is to address a novel control technique for stability and transparency analysis of bilateral telerobotic systems in the presence of data loss and time delay in the communication channel. Different control strategies have been reported to compensate the effects of time delay in the communication channel;however, most of them result in poor performance under data loss. First, a model for data loss is proposed using a finite series representation of a set of periodic continuous pulses.To improve the performance and data reconstruction, a holder circuits is also introduced. The passivity of the overall system is provided via the wave variable technique based on the proposed model for the data loss. The stability analysis of the system is then derived using the Lyapunov theorem under the time delay and the data loss. Finally, experimental results are given to illustrate the capability of the proposed control technique.     

基于前馈及反馈补偿的高性能直线伺服系统

数控机床用直线电动机在工作过程中,推力波动、负载扰动和非线性摩擦等各种扰动因素降低了直线伺服的性能。为抑制扰动满足数控机床直线伺服系统速度跟踪性能的要求,在分析永磁直线同步电动机数学模型和各种扰动因素的基础上,引入具有动态递归特性的Elman神经网络,设计出具有前馈及反馈综合补偿效果的复合控制器,不仅可以对各种扰动进行反馈补偿,而且对速度给定信号进行预测前馈补偿控制,提高了直线伺服系统的跟踪精度和响应速度,仿真结果验证了Elman神经网络的动态性能及综合补偿的优点,表明了复合控制方案的有效性和可行性。

Abstract：

Disturbance variations,such as force ripple,load disturbance and nonlinear friction,directly impose on the motor shaft,leading to significant effect on the computer numerical control （CNC） machine tool servo system performance.In order to satisfy the requirements for speed command tracking performance and eliminate the influence of disturbance,on the bases of the analyzing the mathematics model of permanent magnet linear synchronous motor （PMLSM） and disturbance variation,Elman dynamic recurrent Neural Network was introduced and compound controller with feedforward and feedback comprehensive compensation was proposed.The disturbances were compensated by feedback component and reference speed input signal was preview controlled by feedforward component.The tracking performance and respect speed of linear server system were improved.The advantages of the comprehensive compensation and dynamic of Elman NN were proved.The simulation results show that this compound control scheme is feasible and effective.     

汽车ASS与EPS分层协调控制

以提高汽车行驶平顺性和操纵稳定性为出发点,建立了汽车ASS与EPS的整车动力学模型,提出了一种汽车ASS与EPS集成控制的方法。分别设计了ASS子系统模糊控制器与EPS子系统模糊控制器,利用分层协调控制思想建立了上层协调控制器,对两个子系统进行协调控制。仿真结果表明：采用分层协调控制策略控制的ASS与EPS集成系统可使车身垂直加速度、车身俯仰角、横摆角速度、车身侧倾角等性能参数得到优化,汽车行驶平顺性和操纵稳定性有明显改善,提高了整车综合性能。

Abstract：

Vehicle dynamics model of ASS and EPS was built.A coordination control method of vehicle ASS and EPS was presented to improve vehicle ride performance and handling stability.ASS controller and EPS controller were designed separately.The controller of ASS was designed using fuzzy logic control theory and the EPS system was designed using fuzzy logic control theory too.In order to coordinate the two subsystems,an upper coordination controller was set up based on an idea of delaminating control.The simulation results show that layered coordination control strategy can optimize the vehicle performance parameters and the vehicle integrated performance is improved obviously.     

多系统组合导航仿真器设计

通过分析多种导航系统各自的特点,从对惯性导航系统误差状态的可观测性出发,考虑到校正方式的自由选择、滤波算法的不同采用以及信源的有效性检验等因素,建立了多系统组合导航模型,并采用Simulink工具搭建了该系统仿真器模块。仿真器能够自动地将处于工作状态的导航子系统按照最优准则组合起来,不但能够独立地执行,而且可以与其它导航系统仿真器一起集成在RT-LAB实时环境下正确运行。仿真结果表明,在满足精度的前提下,该系统具有导航信息的冗余性、互补性、容错性等良好性能。

Abstract：

By studying on observable of INS error states and the characteristic of each navigation system,considering the choice of the revision way,the adoption of different filtering algorithms and the verification of the information source,a multi-system integrated navigation model was built.The simulator module of this model was constructed by Simulink tools in MATLAB,which could integrate all active navigation subsystems automatically.The simulator not only could execute independently,but also could run accurately on RT-LAB real-time environment combined with other navigation system simulators.The simulation result indicates that the simulator has many good performances which include the flexibility in integration pattern of navigation systems,the redundancy and complementarity of navigation information,the fault tolerance of the whole system,etc.     

Model algorithm control using neural networks for input delayed nonlinear control system

The performance of the model algorithm control method is partially based on the accuracy of the system’s model. It is difficult to obtain a good model of a nonlinear system, especially when the nonlinearity is high. Neural networks have the ability to "learn"the characteristics of a system through nonlinear mapping to represent nonlinear functions as well as their inverse functions. This paper presents a model algorithm control method using neural networks for nonlinear time delay systems. Two neural networks are used in the control scheme. One neural network is trained as the model of the nonlinear time delay system, and the other one produces the control inputs. The neural networks are combined with the model algorithm control method to control the nonlinear time delay systems. Three examples are used to illustrate the proposed control method. The simulation results show that the proposed control method has a good control performance for nonlinear time delay systems.     

Design and application of single-antenna GPS/accelerometers attitude determination system

In view of the problem that the current single-antenna GPS attitude determination system can only determine the body attitude when the sideslip angle is zero and the multiantenna GPS/SINS integrated navigation system is of large volume, high cost, and complex structure, this approach is presented to determine the attitude based on vector space with single-antenna GPS and accelerometers in the micro inertial measurement unit （MIMU）. It can provide real-time and accurate attitude information. Subsequently, the single-antenna GPS/SINS integrated navigation system is designed based on the combination of position, velocity, and attitude. Finally the semi- physical simulations of single-antenna GPS attitude determination system and single-antenna GPS/SINS integrated navigation system are carried out. The simulation results, based on measured data, show that the single-antenna GPS/SINS system can provide more accurate navigation information compared to the GPS/SINS system, based on the combination of position and velocity. Furthermore, the single-antenna GPS/SINS system is characteristic of lower cost and simpler structure. It provides the basis for the application of a single-antenna GPS/SINS integrated navigation system in a micro aerial vehicle （MAV）.     

Model-Based Network Scheduling and Control for Systems over the IEEE 802.15.4 Network

The scheduling and control of a class of wireless networked control system is investigated,whose control loop is closed via a shared IEEE 802.15.4 wireless network. By using a gain scheduler within the packet-based control framework and fitting the delay-dependent gains into a time-delay system model, a less conservative self-triggered approach is proposed to determine the sampling update,which consequently enables the design of two network scheduling algorithms to reduce the communication usage. Numerical and TrueT ime based examples illustrate the effectiveness of the proposed approach in the sense that it reduces greatly the communication usage while maintaining satisfactory control performance.     

软管式自主空中加油飞行控制系统与仿真研究

基于参考观测器的全状态反馈控制方法设计了受油机飞行控制系统,建立了软管式自主空中加油仿真系统,并进行了仿真验证。根据生成的受油机参考跟踪、对接轨迹,通过输出跟踪观测器在线估算前馈控制信号和参考状态量,设计全状态反馈控制器精确跟踪参考状态,解决了受油插头难以近距离跟踪加油锥套并实现精确对接的问题。以某型UCAV为例,设计了基于全状态反馈控制的自主空中加油仿真系统并进行了数字仿真。仿真结果表明,在四种强度阵风干扰下,设计的空中加油仿真系统能实现精确的双机加油设备跟踪与对接,具有良好的动态性能与鲁棒性能。     

自主空中加油输油阶段无人机建模与控制

针对自主空中加油输油阶段无人机位置保持控制问题,将无人机分为飞机本体和油箱两部分,利用变质量系统理论建立了无人机非线性方程,解决了常规模型无法反映出无人机重量、重心变化的问题。控制律设计方面,通过将变化的油箱转化为外界干扰,提出了基于干扰观测器控制（disturbance observer based control, DOBC）的复合控制结构。复合控制器由位置保持控制器和干扰观测器组成,位置保持控制器采用带积分的线性二次型方法,干扰观测器由比例积分观测器和补偿单元构成,并证明了复合控制器的稳定性。仿真结果表明,将该控制器应用于某型高空无人机非线性模型,可有效减小输油过程带来的影响,实现了输油阶段的位置保持控制。     

威胁条件下一类空中加油区域配置方法研究

空中加油区域的部署对顺利完成空中加油作战任务具有十分重要的作用.对存在敌威胁时的空中加油任务,提出了一种基于遗传算法的区域配置方法.通过建立空中加油各飞机的油耗模型、限定方案搜索区域,并将不同的代价通过转换而统一在适应度函数中,建立了区域优化模型,并结合问题的特点设计了合适的染色体编码和遗传算子.最后对模型进行了仿真计算与分析.     

基于双目视觉的空中加油锥套定位与对接控制

针对插头-锥套式自主空中加油对接过程中实时获取加油锥套空间位置及控制导引的问题, 提出了一种结合深度学习(改进的YOLOv4-Tiny)和双目视觉匹配的快速定位方法。通过插入空间金字塔池化(spatial pyramid pooling, SPP)模块和修改部分卷积层结构, 改进后的YOLOv4-Tiny对416×416的输入检测速度达到182 Hz。与原网络相比, 体积减小20.47%, 在测试集上的平均交并比提高5%;制作了加油锥套的缩比模型进行开展视觉定位实验, 实验中平均深度预测误差小于5%, 空间位置预测符合预期。通过引入一种建立在Yolo预测基础上的快速边缘拟合方法, 获得锥套的椭圆形特征。此外, 建立了一种基于投影算子的模型参考自适应控制(model reference adaptive control, MRAC)增广控制器, 在受油机机体坐标系下跟踪锥套目标。仿真结果显示, 受油机在锥套平面中的平均跟踪误差小于加油锥套的捕获半径, 满足对接要求。     

变质量分布硬式加油管建模与反演自适应控制

硬式加油技术适合给大型飞机加油,能与软式加油形成功能互补。研制硬式加油技术,需要解决伸缩管动力学建模与控制问题。在加油机定直平飞的前提下,建立了考虑伸缩管质量分布变化与气动参数不确定性的动力学模型。将不确定性视为复合扰动,采用反馈线性化实现标称系统的解耦,并分别为俯仰与滚转子系统设计了非线性干扰观测器与反演自适应控制器。仿真结果表明,复合控制器在多种不确定性条件下能达到一致的控制效果,控制性能优于常规增稳控制系统。     

基于Bayes方法的飞机压力加油系统优化设计

针对某型飞机地面压力加油系统存在的常用加油量加油时间过长的问题,提出了一种新的系统优化设计方案。基于该型飞机的常用加油方式为有余油的小加油量加油,并充分考虑到机翼油箱组和机身油箱组的不同特点,提出按机翼油箱组和机身油箱组分别单独进行加油系统优化设计。机翼油箱组按照各油箱同时满油的目标设计,机身油箱组采用Bayes优化方法对节流孔径进行优化设计。系统性能的计算结果验证了该方法的有效性。     

GPS/VISNAV integrated relative navigation and attitude determination system for ultra-close spacecraft formation flying

For the improvement of accuracy and better faulttolerant performance, a global position system (GPS)/vision navigation (VISNAV) integrated relative navigation and attitude determination approach is presented for ultra-close spacecraft formation flying. Onboard GPS and VISNAV system are adopted and a federal Kalman filter architecture is used for the total navigation system design. Simulation results indicate that the integrated system can provide a total improvement of relative navigation and attitude estimation performance in accuracy and fault-tolerance.     

新型歼击机空中加油飞行仿真建模研究

空中加油是提高飞机作战能力的重要手段。空中加油模拟训练成了培养飞行员空中加油技术的重要途径。空中加油飞行的数学建模是模拟加油飞行的理论基础，它直接关系到模拟飞行的逼真程度，关系到模拟加油训练的效果。研究了大型授油机尾流的形成和分布特点，分析了受油机在不同位置进入黾流时飞机所受的影响，提出了相应的数学建模方法。同时分析了新型歼击机在加油过程中飞机质量和重心的变化规律和对飞行性能的影响。     

基于多传感器数据融合的移动机器人导航

提出了一个允许机器人在室内环境中沿规划好的路径移动的决策和控制结构.机器人的控制系统包含了应用特定硬件实现的可以并行运行的几个程序.移动机器人的导航子系统利用卡尔曼滤波器,融合由视觉系统与由里程计获得的位置估计值.通过一组超声波传感器实现障碍物检测.实验结果表明,效果良好.     

立体视觉系统的目标可见性及测量精度分析

立体视觉系统对目标的可见性及测量精度问题直接决定了基于立体视觉的飞行器相对导航的成败及导航精度。从立体视觉系统结构出发,对目标的可见性及测量精度问题进行了研究。分析了目标可见性及系统测量精度的影响因素|推导了相机参数、立体视觉系统结构参数及目标特征位置等因素对视觉盲区、有效视场宽度和目标可分辨性的约束公式|建立了以上各因素对立体视觉系统相对导航测量精度影响的模型公式,并进行了仿真分析。仿真结果可用于飞行器相对导航中立体视觉系统结构的优化设计。