摘要：本文旨在研究用参考模型自适应控制理论设计一种导弹控制器 ,重点介绍了时变参考模型设计过程。参考模型由根据经典控制理论确定的定常参数跟随模型和反馈环节组成 ,并用最优理论完成时变参考模型的设计 ,使得对象在最短的时间内达到所给定的状态。给出采用时变模型参考自适应控制的制导系统的数字仿真结果。

摘要：目的　研究提高激光传输指令系统抗干扰性能的技术； 方法　用软判决方法实现同步捕获；选用（２４，１２）扩展Ｇｏｌａｙ 码并用软判决方法译码；设计了一种能模拟激光传输信道干扰特性和指令传输过程的试验装置；结果　仿真试验得到的平均误码率较小； 结论所述技术方案可以提高激光传输指令系统抗干扰性能；

摘要：The controller design and digital simulation for the hyper velocity kinetic energy missile is investigated. A mathematical model of the trajectory deviation from the line of sight was established, the guidance closed loop was compensated with a phase advance lag corrective network, a selecting algorithm of the attitude control motors used to steer the missile's attitude was presented. In the presence of a wide variety of disturbances the results of digital simulation are satisfactory to circular error probability(CEP) being less than 0 5?m. The steering scheme utilizing attitude control motors as actuators to control the attitude of the missile is feasible.

摘要：A major motivation for this work is to investigate a method of computer simulation for compensating fixed pattern noise of the infrared focal plane arrays. A mathematical model of the output signal of focal plane array was established; a compensating algorithm utilizing reference source was derived and simulating programs were designed. The images of compensating process verify the influence of nonuniformity of responsibility and offset on fixed pattern noise. The result show that simulating method of investigating compensation technology for focal plane arrays is feasible, the generated images and methods can be used to the study of image recognition.

摘要：采用自适应控制理论与经典控制理论相结合的方案 ,用 Popov超稳定理论设计了模型参考自适应控制 (MRAC)系统 ,给出数字仿真结果。