ID 原文 译文
26605 以任务执行总代价、目标毁伤程度和任务执行时间为评价指标，建立目标函数模型； Tasks performed by the total cost, target damage degree and the task execution time as evaluation index, objective function model is set up;
26606 最后，将UAV的种类和数量视为实验因素和水平，研究基于正交实验设计的编队最优配系方案选择方法。 Finally, the amount and type of UAV as experimental factors and levels, research based on the orthogonal experiment design method of formation of the optimal match of scheme selection.
26607 实验结果表明，针对特定的任务要求，该方法可以依据现有的资源条件，得出最优的编队编组策略。 The experimental results show that, for a specific mission requirements, the method can be based on the existing resources conditions, it is concluded that the optimal formation marshalling strategy.
26608 针对时变频率选择性信道下的单载波编码传输系统，提出了基于变分推理的低复杂度Turbo频域均衡与信道估计联合迭代算法。 For single carrier under time-varying frequency selective channel coding transmission system, based on the variational inference Turbo low complexity frequency-domain equalization and joint iterative channel estimation algorithm is proposed.
26609 所设计的软输入软输出检测器和子块间干扰抵消器能统一处理信道估计误差的影响。 The designed soft input soft output between detector and sub-block interference canceller theory can solve the influence of channel estimation error.
26610 通过分析接收信号因子图，提出了算法实现的双迭代结构，内迭代完成联合频域均衡与软信道估计，外迭代进行软干扰抵消和解码。 Through the analysis of received signal factor, puts forward the algorithm of double iterative structure, inner iteration soft joint frequency domain equalization and channel estimation, the iterative soft interference offset and decoding.
26611 仿真结果表明，所提出算法的误码率性能和对叠加训练信号强度的稳健性均优于具有相似复杂度的期望最大化方案。 The simulation results show that the ber performance of the proposed algorithm and the robustness of superposition signal strength training solutions than expectation maximization with similar complexity.
26612 在深入分析中心折反射全景相机成像原理的基础上，提出了一种测量旋翼共锥度的新方法。 In the center of the in-depth analysis of catadioptric panoramic camera imaging principle, on the basis of proposed a new method to measure the rotor common taper.
26613 用安装在直升机桨毂上与旋翼同步旋转的折反射全景相机获取直升机3片桨叶的全景图像。 Installed on the helicopter hub and rotor synchronous rotation catadioptric panoramic camera helicopter 3 blade panoramic images.
26614 根据桨叶上标定块角点坐标与全景图像坐标对应关系，给出了标定块相对于全景相机的外参数计算方法，推导了一组根据平面标定块位置参数计算旋翼共锥度的公式。 According to the calibration blocks on the blade Angle of point coordinates, the corresponding relationship between a panoramic image coordinates are given relative big-picture camera external parameters calculation method of calibration block, a group was deduced according to the plane calibration blocks position parameter calculation formula of rotor common taper.