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《中国航空学报》2020,33(11):2864-2876
The increasing gross weight of electric Unmanned Aerial Vehicle (UAV) poses a challenge in practical applications. The range and endurance of the electric UAV are limited by the fixed mass of the battery package. In this work, a design optimization method for the battery package topology of small electric UAV is proposed to enhance the performance. To improve the accuracy of the method, the dynamic battery model and simplified electric component models are presented. These models are utilized by the trajectory optimization method, which takes the dynamic characteristic into consideration to calculate the aircraft performance. The direct optimal control method is used for solving the trajectory optimization problem, and this method is tested on a small blended-wing-body electric aircraft. The test result shows that the range and energy-consumption are mainly influenced by the parallel topology of the battery package, while the flight time in climb phase is more sensitive to the series topology. It is deduced that the range- and energy-optimal design points can be considered concurrently in design optimization. The work proves the feasibility of integrating the trajectory optimization and battery package design. 相似文献
134.
《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2014,53(2):219-225
The Ionospheric F2-layer peak parameters response to a magnetic storm had been investigated over Ilorin, Nigeria (Lat. 8:53°N, Long. 4.5°E, dip angle, −2.96°), Jicamarca, Peru (11.95°S, 76.87°W, dip angle, 0.8°) and Hermanus, South Africa (34.42°S, 19.22°E, dip angle, −60.77°), using percentage enhancement/depletion values. Our results showed an enhancement in NmF2 at all of these stations. Averagely, pre-noon and post-noon peaks are highest at Ilorin during quiet time. The similar pattern observed for quiet condition between Ilorin and Jicamarca was due to their latitudinal positions. For disturbed NmF2 condition, Jicamarca and Ilorin recorded higher peaks at nighttime than during the daytime for the storms main phase, and the reverse over Hermanus. The nighttime and daytime increases were observed respectively at Ilorin and Hermanus during the recovery period. The hmF2 variation recorded higher enhancement at Jicamarca during the daytime and at Hermanus at nighttime during the main phase. During the recovery phase, the highest enhancement was recorded during the daytime at Jicamarca, and over Hermanus at nighttime. These observations find their explanation in the magnetospheric current, solar wind and E × B drift. 相似文献
135.
K.L. Aplin B.J. Kent C.M. Collingwood L. Wang R. Stevens S.E. Huq A. Malik 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2011
Spacecraft neutralisers are required as part of the ion propulsion system for accurate station keeping in fundamental physics missions. This paper describes the use of thin layers of insulating materials as coatings for the gated silicon field emitter array structure used in a spacecraft neutraliser. These thin coatings are postulated to reduce power consumption and reduce overheating. The power consumption and lifetime of aluminium nitride and amorphous hydrogenated diamond-like carbon coatings have been tested by current–voltage and endurance tests. Diamond-like carbon coatings were promising, performing better in endurance tests than uncoated samples, but further work is required to characterise the coating’s physical properties and its effects on field emission. The thermal conductivity of the coating material had little effect on measured sample lifetimes. Aluminium nitride had reduced power consumption compared to diamond-like carbon coated and uncoated samples. A thin (∼5 nm) layer of aluminium nitride was found to be optimal, meeting European Space Agency specifications for the neutraliser engineering model. 相似文献
136.
自励模式霍尔推力器设计 总被引:1,自引:1,他引:0
为实现P70霍尔推力器自励模式稳定放电运行,分别设计了满足自励模式放电要求的磁路和电路。其磁路设计是基于霍尔推力器他励运行模式最优放电性能参数和磁势不变原理,采用FEMM有限元磁场计算软件建模,将推力器内铁心半径由7 mm减至4 mm,可得到满足自励模式运行要求的优化磁场。针对电磁线圈串入主放电回路不同位置对放电的影响,考虑电磁线圈绝缘要求,提出将电磁线圈串入放电电源负极性端,整体电路设计可使放电可靠。性能对比实验表明,自励模式与他励模式性能接近,在放电电压为420V时,自励模式最高效率达到61%。自励模式实验获得了稳定放电,且放电电流低频振荡幅值很小。 相似文献
137.
海上动态条件下静电陀螺监控器启动技术 总被引:2,自引:0,他引:2
静电陀螺监控器在航天测量船列装是该设备在国内首次被应用于大型水面舰艇。在此之前其设计方案以及启动策略全部针对于水下舰艇,对于航天测量船而言没有任何经验可以借鉴。因此,探索静电陀螺监控器在海上动态条件下的高精度启动技术成为了当前该设备在航天测量船应用中的主要问题。针对该问题,通过分析静电陀螺监控器启动的关键过程,结合设备工作原理,重点对海上动态条件下静电陀螺监控器的启动技术和相关参数进行了研究,实现了静电陀螺监控器在海上动态条件下的高精度启动。该技术目前已经成熟并且成功应用于测量船测控任务。 相似文献
138.
M.V. Klimenko V.V. Klimenko K.G. Ratovsky L.P. Goncharenko 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2011
In this paper, we use the modified GSM TIP model to explore how the thermosphere–ionosphere system in the American longitudinal sector responded to the series of geomagnetic storms on September 9–14, 2005. Comparison of modeling results with experimental data at Millstone Hill, USA (42.6°N, 71.5°W), Ramey, Puerto Rico (18.3°N, 66.8°W) and Jicamarca, Peru (11.9°S, 76.9°W) has shown a good agreement of ionospheric disturbances in the F-region maximum height. We examine in detail the formation mechanisms of these disturbances at different latitudes and describe some of the important physical processes affecting the behavior of the F-region. In addition, we consider the propagation of thermospheric wind surge and the formation of additional layers in the low-latitude ionosphere during geomagnetic storms. 相似文献
139.
三月的苏州花红柳绿、春意融融 ,但我们无暇领略小桥、流水、人家的水乡风情 ,直奔苏州高新技术园区。坐落在园区中心地段的苏州沙迪克三光机电有限公司就是我们此次苏州之行的访问对象 ,宽敞明亮的厂房、整齐有序的装配线、统一着装的员工和好客的主人预示着我们将会有一次愉快和轻松的采访。颇有学者风范、侃侃而谈的包志书董事长向我们说起电加工行业的龙头老大———沙迪克三光的昨天、今天和明天。 相似文献
140.