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排序方式: 共有187条查询结果,搜索用时 171 毫秒
41.
《中国航空学报》2020,33(6):1683-1691
Unmanned Aerial Vehicles (UAVs) have been getting more and more popular in both civil and military arena. Similar to manned aircraft, their propulsion systems or engines emit harmful gases such as nitrogen oxides. Since UAVs have different mission profiles and operational parameters than manned aircraft, it is worthy to investigate their NOx emissions. Therefore, in this study, NOx emissions of a turbofan powered UAV for complete flight cycle was calculated and optimized within a range of altitude and speed parameters. NOx emissions were calculated based on ICAO ground test data and corrected to any speed and altitude during flight legs using both Boeing Fuel Flow Method 2 and DLR Fuel Flow Method. Total NOx emissions were calculated for complete flight cycles for different altitude and speed parameters. Numerical results were presented graphically and additionally optimization studies were conducted. Optimization studies include determination and comparison of speed and altitude for minimum NOx emissions by the two fuel flow methods and maximum loiter time achievable by UAV. 相似文献
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Y. Wu S.G. Jin Z.M. Wang J.B. Liu 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2010
The detection and repair of the cycle slip or gross error is a key step for high precision global positioning system (GPS) carrier phase navigation and positioning due to interruption or unlocking of GPS signal. A number of methods have been developed to detect and repair cycle slips in the last two decades through cycle slip linear combinations of available GPS observations, but such approaches are subject to the changing GPS sampling and complex algorithms. Furthermore, the small cycle slip and gross error cannot be completely repaired or detected if the sampling is quite longer under some special observation conditions, such as Real Time Kinematic (RTK) positioning. With the development of the GPS modernization or Galileo system with three frequencies signals, it may be able to better detect and repair the cycle slip and gross error in the future. In this paper, the cycle slip and gross error of GPS carrier phase data are detected and repaired by using a new combination of the simulated multi-frequency GPS carrier phase data in different conditions. Results show that various real-time cycle slips are completely repaired with a gross error of up to 0.2 cycles. 相似文献
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针对短基线动态相对定位中快速解算整周模糊度的难题,提出了一种新的方法——GPS单历元解算整周模糊度。文中对相关的观测方程、载波相位的观测精度、真假解的识别等问题进行了详细讨论。试验证明,该方法正确、可靠,解决了快速解算整周模糊度这个难题,克服了传统方法需要进行静态初始化等问题。将该方法应用在车辆、舰船等移动载体上,可以实现真正意义上的实时动态相对定位,具有重要的应用价值。 相似文献
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GPS载体姿态测量中的LAMBDA方法研究 总被引:8,自引:0,他引:8
研究了采用双基线方案测量载体的姿态,利用 GPS载波相位干涉测量基线矢量,引入 LAMBDA法解算整周模糊度,由 CPU时间图可以看出这种方法能快速而准确地解算整周模糊度,对于实时姿态测量(RAD)系统具有很好的应用价值。 相似文献
48.
Siyao Wang Bofeng Li Xingxing Li Nan Zang 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2018,61(1):385-401
Integer ambiguity fixing with uncalibrated phase delay (UPD) products can significantly shorten the initialization time and improve the accuracy of precise point positioning (PPP). Since the tracking arcs of satellites and the behavior of atmospheric biases can be very different for the reference networks with different scales, the qualities of corresponding UPD products may be also various. The purpose of this paper is to comparatively investigate the influence of different scales of reference station networks on UPD estimation and user ambiguity resolution. Three reference station networks with global, wide-area and local scales are used to compute the UPD products and analyze their impact on the PPP-AR. The time-to-first-fix, the unfix rate and the incorrect fix rate of PPP-AR are analyzed. Moreover, in order to further shorten the convergence time for obtaining precise positioning, a modified partial ambiguity resolution (PAR) and corresponding validation strategy are presented. In this PAR method, the ambiguity subset is determined by removing the ambiguity one by one in the order of ascending elevations. Besides, for static positioning mode, a coordinate validation strategy is employed to enhance the reliability of the fixed coordinate. The experiment results show that UPD products computed by smaller station network are more accurate and lead to a better coordinate solution; the PAR method used in this paper can shorten the convergence time and the coordinate validation strategy can improve the availability of high precision positioning. 相似文献
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许敏 《民用飞机设计与研究》2014,(1):68-77
经济性对民机项目商业成功至关重要,概述了民机项目定费用设计的起源和基本概念,分别讲述研制费用的估算方法,设计经济性对单机成本的影响,设计经济性对运营成本的影响,总结出定费用设计是民机项目成本控制的关键。 相似文献
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基于协同优化方法,建立了面向成本的飞机结构优化设计模型.该模型不同于传统的结构设计中以质量最小或结构效率最大为优化目标,而是以寿命周期成本为目标,通过相同的结构尺寸变量将结构质量与制造成本联系起来.其中以重量表征油耗成本,寿命周期成本模型被简化为制造成本和油耗成本的函数.在iSIGHT优化平台实现了这一结构协同优化的过... 相似文献