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971.
传统最优控制航迹规划一般以逆风精确着陆、控制能量小为优化目标,但传统最优控制的操纵过程一般是一条连续变化的曲线,工程上不易实施;与之相比,传统分段航迹规划操纵简单,工程上容易实施,能实现逆风精确着陆的目标,但控制能耗大。为了兼顾逆风精确着陆、能耗低和控制操作简单等目标,提出了一种基于梯度下降法的翼伞最优分段航迹规划方法。该方法将控制变量参数化,将逆风精确着陆、控制能耗小、能实现避障等多目标优化问题转化为加权单目标优化问题,并通过梯度下降法求解得到分段常值最优归航航迹。所提算法与基于伪谱法的最优控制规划航迹和基于遗传算法的分段规划航迹进行了对比,算法仿真结果表明本文提出的最优分段航迹规划法既可以实现着陆精度高、控制能量小、逆风着陆和避障的优化目标,同时规划的航迹又由分段常值实现控制,工程上容易实施,兼顾了最优控制航迹规划和分段航迹规划的优点。 相似文献
972.
973.
974.
针对人工免疫木马检测中检测器的冗余,检测过程中成熟检测器和记忆检测器在检测到自我抗原或年龄过大时,被直接删除造成的非我信息资源丢弃等问题,引入限次变异对检测器的生成进行改进,提出将随机生成的检测器在自我耐受后,再与已有合格检测器匹配,对与已有合格检测器匹配的检测器进行限次变异;而检测到自我抗原或年龄过大的检测器同样进行限次变异的方法。实验结果表明,这种方法能准确而快速地检测已知和未知木马。 相似文献
975.
The average likelihood ratio detector is derived as the optimum detector for detecting a target line with unknown normal parameters in the range-time data space of a search radar, which is corrupted by Gaussian noise. The receiver operation characteristics of this optimum detector is derived to evaluate its performance improvement in comparison with the Hough detector, which uses the return signal of several successive scans to achieve a non-coherent integration improvement and get a better performance than the conventional detector. This comparison, which is done through analytic derivations and also through simulation results, shows that the average likelihood ratio detector has a better performance for different SNR values. This result is justified by showing the disadvantages of the Hough method, which are eliminated by the optimum detector. To have an estimate for the location of the detected target line in the optimum detection method as the Hough method, which detects and localizes the target lines simultaneously, we present the maximum a posteriori probability estimator. The estimation performance of the two methods is then compared and it is shown that the maximum a posteriori probability estimator localizes the detected target lines with a better performance in comparison with the Hough method. 相似文献
976.
发动机防冰支板水滴撞击特性的数值研究 总被引:5,自引:2,他引:3
在对发动机防冰支板附近的流场进行计算的基础上,使用离散相模型在拉氏坐标下模拟了该流场中过冷水滴的运动轨迹,对发动机防冰支板的水滴撞击特性进行了研究.研究表明,水滴撞击极限、总收集系数和局部收集系数随飞行高度、来流速度及水滴直径的增加而增大. 相似文献
977.
对色行器落角与撞击时间控制相关问题进行了综述,包括带落角约束的导引问题、带时间约束的导引问题、带落角与时间约束的导引问题、剩余时间估计问题和欠驱动系统的轨迹跟踪控制问题。针对速度不确定飞行器落角与时间控制问题,从航路规划的角度提出了几个值得进一步研究的问题。 相似文献
978.
P. Jakobsson D. Malesani J. Hjorth J.P.U. Fynbo B. Milvang-Jensen 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2011
We describe the current status and recent results from our Swift/VLT legacy survey, a VLT Large Programme aimed at characterizing the host galaxies of a homogeneously selected sub-sample of Swift GRBs. The immediate goals are to determine the host luminosity function, study the effects of reddening, determine the fraction of Lyα emitters in the hosts, and obtain redshifts for targets without a reported one. The main effort so far has been the definition of a very carefully selected sample, obeying strict and well-defined criteria: 68 targets in total. Among the preliminary results is a large optical detection rate, the lack of extremely red objects (only one possible case in the sample) and an update of the Swift GRB redshift distribution with 〈z〉∼2.0. 相似文献
979.
Kazunori Ogohara Takehiko Satomura 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2011
Using a Martian general circulation model (GCM), regions favorable for expansion of dust storms on Mars are identified. Dust transport simulations for the northern fall provide global maps of dust expansibility. These global maps show that dust injected from certain areas in the northern mid-latitudes tends to spread widely within a few days. The high expansibility of dust in such areas results from thermal tides, baroclinic waves, and quasi-stationary disturbances. Dust injected into the vast regions around Tharsis and the Sirenum–Aonia regions also tends to spread extensively. However, dust expansion around these two regions largely depends on the local time of dust injection. On the other hand, dust injected at high latitudes in either hemisphere does not spread extensively. Such global maps indicating regions favorable for dust storm expansion are a clue to understanding the expansion processes and climatology of great dust storms on Mars. 相似文献
980.
针对敏捷卫星的三轴大角度机动控制要求,给出了一种基于轨迹规划的敏捷卫星姿态机动方法.根据目标姿态和当前姿态,按照欧拉轴-角方式,沿特征主轴设计了最小路径的机动轨迹,并采用四个单框架控制力矩陀螺(SGCMG)组成的“金字塔”构型的控制力矩陀螺群(CMGs)进行了大角度机动控制的数学仿真,验证了方法的可行性. 相似文献