舰载飞机着舰精确轨迹控制研究

针对舰载机着舰过程的精确航迹控制要求,利用现有机上的控制设备,采用系统综合设计的方法,给出了两种航迹控制系统———风参考航迹控制系统和惯性参考航迹控制系统,通过仿真分析,给出了系统的性能差异。     

一种新型的分布式数据采集器(一)

介绍了一种新型的分布式智能数据采集系统──ALPHA900系列数据采集器。该采集器由中国航空工业总公司第三0四研究所与英国ADAS公司联合设计研制。它集中了90年代采集器的优点，如可变字长、可编程智能前端、带温度补偿的连接器、可脱机工作等，并为突出各自功能形成系列。该采集器已成功地投入了工业生产，并且应用于工业过程监测、条件监测或加工监测。该系统使用价格低廉的RS485网络，各种型号模块提供了精确的温度、压力、应变及数字事件和频率等数据的测量及控制，并有相当突出的性能价格比。     

飞机纵向杆力—杆位移曲线的自动检测

提出了飞机纵向杆力－杆位移曲线的一种自动化检测方法－机器手检测法。首先简述了机器手的组成及原理，然后讨论了杆力、杆位移的自动检测及纵向杆力－杆位移曲线的绘制与处理方法，最后利用该机器手对两种飞机进行了实际检测，并对检测曲线进行了精度分析。结果表明，机器手检测法经济简单、自动化程度和精度较高，是检测飞机纵向杆力－杆位移曲线的一种行之有效的方法。同时，该检测仪也适用于各种飞机的检测，对飞机横向杆力－杆     

论折旧基金的补偿性——兼析折旧基金具有两重性的观点

作者根据马克思的劳动价值理论现点,结合我国经济的实践,对折旧基金的补偿性质进行了较深入的分析。     

Design and implementation of five-axis transformation function in CNC system

To implement five-axis functions in CNC system, based on domestic system Lan Tian series, an improved design method for the system software structure is proposed in this paper. The numerical control kernel of CNC system is divided into the task layer and the motion layer. A five-axis transformation unit is integrated into the motion layer. After classifying five-axis machines into different types and analyzing their geometry information, the five-axis kinematic library is designed according to the abstract factory pattern. Furthermore, by taking CA spindle- tilting machine as an example, the forward and the inverse kinematic transformations are deduced. Based on the new software architecture and the five-axis kinematic library, algorithms of RTCP （rotation tool center point control） and 3D radius compensation for end-milling are designed and realized. The milling results show that, with five-axis functions based on such software struc- ture, the instructions with respect to the cutter＇s position and orientation can be directly carried out in the CNC system.     

载体角运动对旋转捷联惯导误差的影响分析

旋转捷联惯导系统采用旋转调制误差补偿技术对陀螺仪和加速度计误差进行调制,可以提高系统导航精度。在简要分析旋转调制误差补偿机理基础上,研究了单轴旋转方案中载体常值旋转和周期旋转2种角运动模式对导航误差的影响。结果表明：载体特定角运动对旋转捷联惯导的误差补偿效果有一定影响,且单轴正反转停方案中误差补偿效果所受影响相对较小。     

一种高精度天线转台的实时补偿方法

天线转台是天线罩电性能测试系统的重要组成部分,对精度要求很高.由于磁栅传感器磁栅特性和安装等原因,其精度往往达不到厂家标称精度,需要进行补偿以满足系统要求.本文详细分析了造成磁栅测量精度达不到标称精度的原因,并针对主要原因提出了一种软件实时补偿算法,详细论述了补偿原理,通过测量转台绝对定位精度,验证了该实时补偿算法具有...     

Friction compensation for low velocity control of hydraulic flight motion simulator: A simple adaptive robust approach

Low-velocity tracking capability is a key performance of flight motion simulator (FMS), which is mainly affected by the nonlinear friction force. Though many compensation schemes with ad hoc friction models have been proposed, this paper deals with low-velocity control without friction model, since it is easy to be implemented in practice. Firstly, a nonlinear model of the FMS middle frame, which is driven by a hydraulic rotary actuator, is built. Noting that in the low velocity region, the unmodeled friction force is mainly characterized by a changing-slowly part, thus a simple adaptive law can be employed to learn this changing-slowly part and compensate it. To guarantee the boundedness of adaptation process, a discontinuous projection is utilized and then a robust scheme is proposed. The controller achieves a prescribed output tracking transient performance and final tracking accuracy in general while obtaining asymptotic output tracking in the absence of modeling errors. In addition, a saturated projection adaptive scheme is proposed to improve the globally learning capability when the velocity becomes large, which might make the previous proposed projection-based adaptive law be unstable. Theoretical and extensive experimental results are obtained to verify the high-performance nature of the proposed adaptive robust control strategy.     

Precise control of a magnetically suspended double-gimbal control moment gyroscope using differential geometry decoupling method

Precise control of a magnetically suspended double-gimbal control moment gyroscope (MSDGCMG) is of vital importance and challenge to the attitude positioning of spacecraft owing to its multivariable, nonlinear and strong coupled properties. This paper proposes a novel linearization and decoupling method based on differential geometry theory and combines it with the internal model controller (IMC) to guarantee the system robustness to the external disturbance and parameter uncertainty. Furthermore, by introducing the dynamic compensation for the inner-gimbal rate-servo system and the magnetically suspended rotor (MSR) system only, we can eliminate the influence of the unmodeled dynamics to the decoupling control accuracy as well as save costs and inhibit noises effectively. The simulation results verify the nice decoupling and robustness performance of the system using the proposed method.     

复杂环境下多无人机轨迹姿态协同控制

考虑多无人机在实际飞行过程中的避障需求，在建立面向控制的四旋翼无人机轨迹姿态模型基础上，为克服传统多无人机为每架无人机规划轨迹的不足，研究了基于多无人机中心点的轨迹设计策略。进一步，考虑避障约束，基于半定规划进行迭代区域扩张完成了多无人机的安全飞行区域及队形设计。在此基础上，基于干扰补偿策略为每架无人机设计了协同控制器，最终确保了多无人机在多障碍环境下的安全飞行。