ID 原文 译文
49537 首先利用微动参数构建相位补偿因子，之后对时间距离像进行三维搜索，进而实现进动目标的三维成像。 First using micro parameter to build phase compensation factor, after the time distance like 3 d search, thus achieving precession 3-d imaging.
49538 最后通过仿真实验验证了所提方法的有效性，同时仿真分析了微动参数估计误差对成像的影响。 Finally, the effectiveness of the proposed method is verified by simulation experiments, and the simulation analysis of the micro parameters estimation error effect on imaging.
49539 针对传统制导和控制分开设计在拦截高速机动目标时的不足，给出了一种反演滑模一体化制导控制算法。 Against the traditional separate design of guidance and control in intercepting high maneuvering target, an inversion sliding mode integration guidance control algorithm is given.
49540 首先利用微分几何理论，建立了一体化制导控制模型; Using the theory of differential geometry, the first integration guidance control model is established;
49541 然后根据平行接近原理，基于滑模控制和反演法，设计了一种反演滑模控制的导弹制导控制一体化算法; Then according to the principle of parallel approach, based on sliding mode control and inversion method, we design an inversion of sliding mode control of the missile guidance control integration algorithm;
49542 最后基于Lyapunov理论证明了系统的稳定性。 Finally the stability of the system is proved based on Lyapunov theory.
49543 数值仿真结果表明，所给出的一体化制导控制方法能够克服未建模的不确定性和目标机动干扰，具有较强的鲁棒性。 Given by the numerical simulation results show that the integrated guidance control method can overcome the unmodeled uncertainties and target maneuver interference, has strong robustness.
49544 当前网络和信息技术的发展为C4ISR(command，control，communication computer，intelligence，surveillance，reconnaissance，C4ISR)系统的灵活性提出了更大的挑战。 The current network and the development of information technology for C4ISR (command, control, communication computer, intelligence, surveillance, reconnaissance, C4ISR) the flexibility of the system proposes a bigger challenge.
49545 灵活性存在于C4ISR系统的多个方面，其中结构灵活性是系统灵活性的支撑。 Flexibility exists in various aspects of C4ISR system, including structure flexibility is the flexibility of the supporting system.
49546 首先明确了系统结构灵活性的基本内涵， First clear the basic connotation of the system structure flexibility,