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621.
亚跨超风洞现代试验设计方法研究 总被引:2,自引:0,他引:2
开展了基于现代试验设计方法(MDOE)的亚跨超风洞试验研究,以八号标模尾翼为试验对象研究其气动特性,采用同时改变攻角-侧滑角的多变量方法,而不是传统的单变量(OFAT)方法进行试验。对自变量攻角和侧滑角进行试验设计(DOE),应用响应面法建模,用IV-最优方法对测量点分布进行设计。在FD-12亚跨超风洞完成了试验,并和传统的OFAT方法结果进行比较分析。结果表明:MDOE方法获得的数据和传统的OFAT方法的数据吻合很好;MDOE采集样点数减少了46%,吹风的时间比OFAT减少30%左右,提高了风洞试验效率,缩短了试验周期;MDOE试验方法可以给出设计空间内任意给定自变量对应的响应值及其置信区间。 相似文献
622.
To find a way of loads analysis from operational flight data for advanced aircraft,maneuver identification and standardization jobs are conducted in this paper. For thousands of sorties from one aircraft, after studying the flight attitude when performing actions, the start and end time of the maneuvers can be determined. According to those time points, various types of maneuvers during the flight are extracted in the form of multi-parameters time histories. By analyzing the numerical range and curve shape of those parameters, a characteristic data library is established to model all types of maneuvers. Based on this library, a computer procedure using pattern-recognition theory is programmed to conduct automatic maneuver identification with high accuracy. In that way, operational loads are classified according to maneuver type. For a group of identified maneuvers of the same type, after the processes of time normalization, trace shifting, as well as averaging and smoothing, the idealization standard time history of each maneuver type is established.Finally, the typical load statuses are determined successfully based on standard maneuvers. The proposed method of maneuver identification and standardization is able to derive operational loads effectively, and might be applied to monitoring loads in Individual Aircraft Tracking Program(IATP). 相似文献
623.
Automatic dependent surveillance-broadcast (ADS-B) systems can broadcast satellitebased aircraft position, identification, etc., periodically, and are now on track to replace radar to become the backbone of next-generation air traffic management (ATM) systems. However, ADS-B systems suffer severe cyber-security problems due to the broadcast-type data link and the lack of designed-in security measures. Especially, since ADS-B messages are unauthenticated, it is easy to insert fake aircraft into a system via spoofing or insertion of false messages. Unfortu- nately, the authentication for ADS-B messages has not yet been well studied. In this paper, based on identity-based signature with message recovery (IBS-MR), an efficient broadcast authentication scheme for ADS-B messages is proposed. The security analysis demonstrates that the scheme can achieve authenticity and integrity of ADS-B broadcast messages, as well as adaptive evolution of broadcasters' private keys. The performance evaluation shows that the scheme is computationally efficient for typical avionics devices with limited resources. Furthermore, the scheme achieves low communication overhead since broadcast messages can be recovered from signatures, and thus it is suitable for low-bandwidth ADS-B data link. 相似文献
624.
The application of high-performance imaging sensors in space-based space surveillance systems makes it possible to recognize space objects and estimate their poses using vision-based methods. In this paper, we proposed a kernel regression-based method for joint multi-view space object recognition and pose estimation. We built a new simulated satellite image dataset named BUAA-SID 1.5 to test our method using different image representations. We evaluated our method for recognition-only tasks, pose estimation-only tasks, and joint recognition and pose estimation tasks. Experimental results show that our method outperforms the state-of-the-arts in space object recognition, and can recognize space objects and estimate their poses effectively and robustly against noise and lighting conditions. 相似文献
625.
Optimal guidance of extended trajectory shaping 总被引:3,自引:1,他引:2
To control missile's miss distance as well as terminal impact angle, by involving the timeto-go-nth power in the cost function, an extended optimal guidance law against a constant maneuvering target or a stationary target is proposed using the linear quadratic optimal control theory.An extended trajectory shaping guidance(ETSG) law is then proposed under the assumption that the missile-target relative velocity is constant and the line of sight angle is small. For a lag-free ETSG system, closed-form solutions for the missile's acceleration command are derived by the method of Schwartz inequality and linear simulations are performed to verify the closed-form results. Normalized adjoint systems for miss distance and terminal impact angle error are presented independently for stationary targets and constant maneuvering targets, respectively. Detailed discussions about the terminal misses and impact angle errors induced by terminal impact angle constraint, initial heading error, seeker zero position errors and target maneuvering, are performed. 相似文献
626.
针对现有飞行器测控系统遥测对接试验周期长、效率低的不足,提出一种异地遥测对接方法.通过构建异地遥测对接系统结构,得到异地遥测对接信号链路模型.基于系统时钟抖动的频率、相位和采样时间表达形式,对异地遥测对接链路中的信号进行了具体推导.在此基础上,从频率和相位2个方面,定量分析了系统时钟抖动对异地遥测对接信号相参性的影响.分析结果表明:对于Ka频段信号,当应答机端异地遥测对接系统的时钟短期频率稳定度优于1×10^-11时,异地遥测对接系统引入的频率抖动△f≤0.6 Hz,相位抖动△φ≤0.075 rad,可认为异地遥测对接信号的相参性不受影响,异地遥测对接可行. 相似文献
627.
628.
X Zhang X B Li S Z Yang S G Li P D Jiang Z H Lin 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2003,32(8):1577-1583
Using the cultured chicken embryonic chondrocytes as a model, the effects of simulated microgravity on the microtubular system of the cellular skeleton, extracellular matrix, alkaline phosphatase activity, intracellular free calcium concentration and mitochondrial ATP synthase activity with its oligomycin inhibition rate were studied with a clinostat. The microtubular content was measured by a flow cytometer. The decrease of microtubular content showed the impairment of the cellular skeleton system. Observation on the extracellular matrix by the scanning electron microscopy showed that it decreased significantly after rotating, and the fibers in the extracellular matrix were more tiny and disorderly than that of the control group. It can be concluded that the simulated microgravity can affect the secreting and assembly of the extracellular matrix. In contrast to the control, there was a time course decrease in alkaline phosphatase activity of chondrocytes, a marker of matrix mineralization. Meanwhile a significant drop in the intracellular calcium concentration happened at the beginning of rotation. These results indicate that simulated microgravity can suppress matrix calcification of cultured chondrocytes, and intracellular free calcium may be involved in the regulation of matrix calcification as the second signal transmitter. No significant changes happened in the mitochondrial ATP synthase activity and its oligomycin inhibition rate. Perhaps the energy metabolism wasn't affected by the simulated microgravity. The possible mechanisms about them were discussed. 相似文献
629.
Zhenhua Jiang Shengyi Liu Dougal R.A. 《IEEE transactions on aerospace and electronic systems》2003,39(3):976-989
A study is presented on the design and testing of spacecraft power systems using the virtual test bed (VTB). The interdisciplinary components such as solar array and battery systems were first modeled in native VTB format and validated by experiment data. The shunt regulator and battery charge controller were designed in Simulink according to the system requirements and imported to VTB. Two spacecraft power systems were then designed and tested together with the control systems. 相似文献
630.
JIN Weiqing Shinichi Yoda Jiang Yuanfang LIANG Xinan PAN Zhilei Shen Guotu Liu Zhaohua 《空间科学学报》2002,22(Z1)
We have investigated experimentally and theoretically the thermocapillary convec tive flow phenomena in a loop-shaped Pt wire heater of KNbO3 (20wt.%) and Li2B4O7 solutions. Optical evaluations in connection with thermocouple measure ments made it possible to get a new type of thermocapillary convective flow in the considered system. To study the kinematical behaviour of thermocapillary convec tion, we have measured the stream flow velocities. In a theoretical analysis, the flow velocity due to the thermocapillary effect alone was estimated by balancing the sur face tension forces by viscous forces. The velocity distribution in the solution near the margin of the heater was obtained, which is in agreement with the experimental result. 相似文献