A very severe nonlinear is presented because flight parameters vary along with the flight condition in the flight of missile which brings much difficulty to the design of control system.
导弹在飞行过程中，其飞行参数随着飞行条件的变化而发生较大变化，呈现严重的非线性，给控制系统的设计带来较大困难。
The key problem is that the decoupling method and the harmonious control should be studied in the missile flight simulator system control.
所以，在大系统控制中，首要问题是研究解耦方法和协调控制。
The method for consistency check of multisensor data by using the probability distance measuring is presented, and it used in CAN bus missile guidance and control system based on multi-IMU.
提出了应用概率距离测量对多传感器信息进行一致性检验的方法，并将此方法引入到基于多惯性测量组合的总线式导弹制导控制系统中。
As a synthesis method in control system, the sliding mode of variable structure control is invariable, and which is its most excellent advantage in the missile attitude control system.
变结构控制作为控制系统的一种综合方法，它的滑动模态具有不变性，这是变结构控制在导弹姿态控制中最突出的优点。
This method are with a high accuracy and real time application, and can be applied in the calculation of allowable launching area of air to air missile in air borne fire control system.
提出了一种确定目标进入角的原理和方法，这种原理和方法具有较高的计算精度和实时性，易于工程实现，可用于机载火力控制系统完成空对空导弹允许发射区计算。
In fact, after the America national missile defense system is deployed on a global scale, the United States can control all other country, of courses, including its friends and Allies.
事实上，美国国家导弹防御系统一旦在全球部署，可使美国能控制世界上所有国家，当然也包括其朋友和盟国。
In this paper, a nonlinear adaptive control scheme for missile control system with mismatched uncertainties is proposed on the basis of RBF neural networks and inverse control technology.
在导弹系统存在非匹配不确定性的情况下，提出了一种基于RBF神经网络和反演控制技术的神经网络自适应导弹控制系统的设计方法。
These conclusions can be used for system design of rotating missile in the attitude control system and selection of structure and pneumatic parameters for supersonic fluidic elements.
所得结论可为旋转弹姿态控制系统的总体设计以及超音速射流元件的结构及气动参数选择提供依据。
In order to enter into the ideal trajectory with minimal energy, the nonlinear thrust vector control and the prediction guidance are adopted in the missile guidance control system.
为使飞行器能在主动段很快地进入到理想弹道上，系统采用了非线性的推力向量控制及预测制导方法。
A design method of adaptive flight control system for certain missile control system is introduced in this paper, in which adaptive control theory can be applied.
针对某型导弹控制系统，通过自适应控制理论的应用，介绍了一种自适应制导控制系统的构建方法。
Optical fiber technology is used in missile control system, which can resolve the electromagnetic interfere, the electric isolation, anti-jamming and so on in control system effectively.
光纤技术用于导弹控制系统中，有效解决了控制系统的电磁兼容、电气隔离、抗干扰等问题，大大提高了导弹控制系统的性能与可靠性。
Microwave phase shifter in phased-array radar, communications, instrumentation, heavy ion accelerator and the missile attitude control system has a broad application prospects.
微波移相器在雷达、通信、仪器仪表、重离子加速器及导弹姿态控制系统中有着广泛的应用前景。
Actuality research station in-out country and production of our team in guidance of missile and control system are discussed. At last, application foreground of this investigation is explained.
总结了国内外在人眼视觉系统方面的研究现状及本课题组对于仿生技术在导弹制导、控制系统中的应用研究的主要内容、已取得的成果以及研究成果的应用前景。
Actuality research station in-out country and production of our team in guidance of missile and control system are discussed. At last, application foreground of this investigation is explained.
总结了国内外在人眼视觉系统方面的研究现状及本课题组对于仿生技术在导弹制导、控制系统中的应用研究的主要内容、已取得的成果以及研究成果的应用前景。
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