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排序方式: 共有590条查询结果,搜索用时 15 毫秒
1.
Robert A. Bettinger 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2021,67(10):3267-3281
A unique logic-based algorithm for atmospheric reentry hemisphere prediction is presented for spacecraft in low-eccentricity, prograde low Earth orbits at altitudes of 300 km and lower. Using two-line element (TLE) data for initial orbit conditions, coupled with coarse estimates for spacecraft aerodynamic characteristics, the algorithm relies on logical disjunction operations based on a dual analysis of histogram and two-weighted Gaussian probability density function (PDF) fits of predicted reentry latitude data. The algorithm requires the execution of a series of parametric simulations to determine the reentry hemisphere for variations in spacecraft aerodynamic coefficients and drag reference area. When implemented, the algorithm yields accurate hemisphere predictions on average 15 days from reentry as demonstrated by historical reentry cases from 1979 to 2018. All reentry cases were selected to demonstrate the algorithm’s ability to deliver accurate reentry hemisphere predictions for spacecraft with varying physical size and mass, and reentering during different periods of solar cycle activity. 相似文献
2.
《中国航空学报》2020,33(4):1154-1165
This paper focuses on the effects of external geometrical modifications on the aerodynamic characteristics of the MQ-1 predator Unmanned Combat Aerial Vehicle (UCAV) using computational fluid dynamics. The investigations are performed for 16 flight conditions at an altitude of 7.6 km and at a constant speed of 56.32 m/s. Two models are analysed, namely the baseline model and the model with external geometrical modifications installed on it. Both the models are investigated for various angles of attack from −4° to 16°, angles of bank from 0° to 6° and angles of yaw from 0° to 4°. Due to the unavailability of any experimental (wind tunnel or flight test) data for this UCAV in the literature, a thorough verification of calculations process is presented to demonstrate confidence level in the numerical simulations. The analysis quantifies the loss of lift and increase in drag for the modified version of the MQ-1 predator UCAV along with the identification of stall conditions. Local improvement (in drag) of up to 96% has been obtained by relocating external modifications, whereas global drag force reduction of roughly 0.5% is observed. The effects of external geometrical modifications on the control surfaces indicate the blanking phenomenon and reduction in forces on the control surfaces that can reduce the aerodynamic performance of the UCAV. 相似文献
3.
S. Narendranath P.S. Athiray P. Sreekumar V. Radhakrishna A. Tyagi B.J. Kellett the CLASS team 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2014
Surface chemistry of airless bodies in the solar system can be derived from remote X-ray spectral measurements from an orbiting spacecraft. X-rays from planetary surfaces are excited primarily by solar X-rays. Several experiments in the past have used this technique of X-ray fluorescence for deriving abundances of the major rock forming elements. The Chandrayaan-2 orbiter carries an X-ray fluorescence experiment named CLASS that is designed based on results from its predecessor C1XS flown on Chandrayaan-1. We discuss the new aspects of lunar science that can be potentially achieved with CLASS. 相似文献
4.
基于L2范数度量的k平面聚类(k-Plane Clustering,k PC)设计思想,本文提出了一种采用L1范数度量的聚类算法。由于在平面更新步骤中,所导出的优化问题是非凸的,文中给出了一种求解方法,即将非凸问题转化为有限个子集上的凸问题,为避免求解多个优化问题导致训练时间过长问题,本文还设计了一种新的优选策略,有限个子集的搜索任务可在线性时间内完成。本文所提出的方法只需要求解k个线性规划,而不再是k PC的求解特征值问题。在人工和UCI数据集上的实验结果表明:基于L1范数平面聚类算法的训练和测试时间更短,且在大多数数据集上均表现出了更好的聚类性能。 相似文献
5.
《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2020,65(1):560-571
The precise point positioning (PPP) technique is widely used in time and frequency applications. Because of the real-time service (RTS) project of the International GNSS Service, we can use the PPP technique for real-time clock comparison and monitoring. As a participant in the RTS, the Centre National d’Etudes Spatiales (CNES) implements the PPPWIZARD (Precise Point Positioning with Integer and Zero-difference Ambiguity Resolution Demonstrator) project to validate carrier phase ambiguity resolution. Unlike the Integer-PPP (IPPP) of the CNES, fixing ambiguities in the post-processing mode, the PPPWIZARD operates in the real-time mode, which is also called real-time IPPP (RT-IPPP). This paper focuses on applying the RT-IPPP for real-time clock comparison and monitoring. We review the principle of real-time clock comparison and monitoring, and introduce the methodology of the RT-IPPP technique. The observations of GPS, GLONASS and Galileo were processed for the experiments. Five processing modes were provided in the experiment to analyze the benefits of ambiguity resolution and multi-GNSS. In the clock comparison experiment, the average reduction ratios of standard deviations with respect to the G PPP mode range from 9.7% to 35.0%. In the clock monitoring experiment, G PPP mode can detect clock jumps whose magnitudes are larger than 0.9 ns. The RT-IPPP technique with GRE PPP AR (G) mode allows for the detection of any clock jumps larger than 0.6 ns. For frequency monitoring, G PPP mode allows detection of frequency changes larger than 1.1 × 10−14. When the RT-IPPP technique is applied, monitoring with GRE PPP AR (G) mode can detect frequency changes larger than 6.1 × 10−15. 相似文献
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8.
针对FCD1软脆光学镜片高效高成品率的精密加工问题,本研究提出了一种使用复合结合剂金刚石丸片的精研加工技术,其金刚石丸片研具采用了金属、树脂和添加剂等复合结合剂。在精研过程中,丸片表层金刚石磨粒对工件的切深一致性避免了工件表面易出现的深划痕,可有效减少后道抛光工序加工时间,从而提高FCD1软脆光学镜片的生产效率和成品率。 相似文献
9.
研究了φ4mm与φ2mm的扩散连接界面缺陷对Ti-6Al-4V合金力学性能的影响。当拉伸载荷方向与缺陷平面平行时,材料的强度与塑性与无缺陷材料相当,这是由于此类缺陷对样品受力截面的面积几乎没有影响。含有φ4mm缺陷试样的拉压疲劳寿命展现出很大的分散性,界面缺陷并未成为裂纹萌生的唯一位置。从表面起裂的样品均处于高寿命区域,而绝大部分从缺陷处起裂的样品均落于低寿命区域。有限元分析表明,当缺陷位于中心位置时其引起的应力集中较小,应力分布梯度较小;缺陷位于边缘位置时,应力集中效应增大。 相似文献
10.
《中国航空学报》2016,(6):1762-1773
L-band digital aeronautical communication system 1 (L-DACS1) is a promising candi-date data-link for future air-ground communication, but it is severely interfered by the pulse pairs (PPs) generated by distance measure equipment. A novel PP mitigation approach is proposed in this paper. Firstly, a deformed PP detection (DPPD) method that combines a filter bank, correlation detection, and rescanning is proposed to detect the deformed PPs (DPPs) which are caused by mul-tiple filters in the receiver. Secondly, a finite impulse response (FIR) model is used to approximate the overall characteristic of filters, and then the waveform of DPP can be acquired by the original waveform of PP and the FIR model. Finally, sparse representation is used to estimate the position and amplitude of each DPP, and then reconstruct each DPP. The reconstructed DPPs will be sub-tracted from the contaminated signal to mitigate interference. Numerical experiments show that the bit error rate performance of our approach is about 5 dB better than that of recent works and is closer to interference-free environment. 相似文献