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《中国航空学报》2020,33(1):191-204
To efficiently and fully utilize aircraft carrier resources, an optimization model is presented to deal with parameter matching between aircraft and carrier in the process of aircraft catapult launch. Based on carrier aircraft longitudinal dynamic equations and theorem of kinetic energy in catapult launch course, the work characteristics of different forces are learned and a theory model of parameter matching is deduced. In view of the uncertainty of the model parameters of the theory model and the low matching accuracy of the approximate model, an optimization model of parameter matching is introduced in line with the structure of theory model and the approximate model and is generated by the proposed immune genetic algorithm. Compared with the original genetic algorithm and immune algorithm, the proposed algorithm has better calculation accuracy and convergence. The calculation results show that the optimization model occupies certain application value of engineering estimation from the comparison with the relevant literature data and has higher precision than the approximate models. The validity of the proposed approach is verified with numerical case study on a carrier based aircraft. 相似文献
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杜文文 《中国空间科学技术》1988,(4)
本文在考虑大气密度(90km高度以下) 随地理纬度、高度及时间(月份)随机变化的基础上,沿卫星的返回轨道建立了随机大气密度的统计模型。并应用该模型产生的随机大气密度样本,进行返回轨道的Monte Corlo法模拟计算。通过对模拟计算得到的返回轨道参数样本的统计处理,本文分析了大气密度变化对卫星返回轨道参数的影响。另外,本文还介绍了近似估计大气密度变化对返回轨道参数影响的影响系数法。 相似文献
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作者提出的变比热正冲波改进解析解,延伸用于马赫数从3到7情况,求出过冲波后全部气动参数,按马赫数间隔为1列表给出。并附列定比热结果误差。同时提出了只取初温到终温平均比热的单比热比k_(12)近似解,平行列出结果及误差。 相似文献
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基于原模图构造的低密度奇偶校验码(LDPC)性能很大程度上取决于扩展算法。为此,提出了一种构造准循环低密度奇偶校验码(QC-LDPC)的新方法。所述算法经过两步扩展得到QC-LDPC:第一步是原模图去重边,在边置换条件的约束下,使扩展所得矩阵局部围长最大化;第二步进行准循环扩展,通过计算机搜索得到规定长度内的所有闭环路径,比较环长和近似环路外信息度得到置换矩阵的最优偏移量,目的是剔除连通性差的短环对码性能的负面影响。对于不存在重边的原模图,则直接进行准循环扩展。仿真结果表明,利用该方法构造的QC-LDPC在译码门限和误码平层两方面都具有优异的性能。 相似文献
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根据火箭发动机的推力公式及空气动力学有关理论,导出在小斜切角喷管内气体流动的特性、推力的变化规律,并给出喷管的设计方法. 相似文献
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The problem of generating optimal paths for curvature-constrained unmanned aerial vehicles (UAVs) performing surveillance of multiple ground targets is addressed in this paper. UAVs are modeled as Dubins vehicles so that the constraints of UAVs' minimal turning radius can be taken into account. In view of the effective surveillance range of the sensors equipped on UAVs, the problem is formulated as a Dubins traveling salesman problem with neighborhood (DTSPN). Considering its prohibitively high computational complexity, the Dubins paths in the sense of terminal heading relaxation are introduced to simplify the calculation of the Dubins distance, and a boundary-based encoding scheme is proposed to determine the visiting point of every target neighborhood. Then, an evolutionary algorithm is used to derive the optimal Dubins tour. To further enhance the quality of the solutions, a local search strategy based on approximate gradient is employed to improve the visiting points of target neighborhoods. Finally, by a minor modification to the individual encoding, the algorithm is easily extended to deal with other two more sophisticated DTSPN variants (multi-UAV scenario and multiple groups of targets scenario). The performance of the algorithm is demonstrated through comparative experiments with other two state-of-the-art DTSPN algorithms identified in literature. Numerical simulations exhibit that the algorithm proposed in this paper can find high-quality solutions to the DTSPN with lower computational cost and produce significantly improved performance over the other algorithms. 相似文献
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本文导出了带挠性伸展附件航天器姿态动力学方程,研究了附件伸展和振动对姿态动力学的影响。对于附件按指数规律伸展情况,以及附件长度的次方随时间线性变化情况,给出了姿态角速率的渐近公式。 相似文献
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王宁 《中国空间科学技术》1990,10(2):52
文章用拟合方法给出了复杂系统的有效度单边近似下限解,可用来计算卫星系统的有效度单边近似下限,并为评估卫星系统的最短寿命提供数据参考。 相似文献
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