无人机系统适航标准剪裁案例分析

无人机系统的使用日益广泛,因此将无人机系统并入到现有的空域管理系统中显得尤为迫切。在技术层面,无人机系统有一系列独特的适航特点。因此,应重点发展针对无人机系统的适航标准与验证。研究了有人驾驶飞行器的适航标准(CS-23),及其通过剪裁后成为专门适用于无人机系统的适航标准(STANAG4671),这将促进无人机系统的技术更加标准化,并有利于国内无人机系统民用适航标准的发展。     

Effect of blade sweep on inlet flow in axial compressor cascades

This paper presents comparative numerical studies to investigate the effects of blade sweep on inlet flow in axial compressor cascades. A series of swept and straight cascades was modeled in order to obtain a general understanding of the inlet flow field that is induced by sweep.A computational fluid dynamics(CFD) package was used to simulate the cascades and obtain the required three-dimensional(3D) flow parameters. A circumferentially averaged method was introduced which provided the circumferential fluctuation(CF) terms in the momentum equation.A program for data reduction was conducted to obtain a circumferentially averaged flow field.The influences of the inlet flow fields of the cascades were studied and spanwise distributions of each term in the momentum equation were analyzed. The results indicate that blade sweep does affect inlet radial equilibrium. The characteristic of radial fluid transfer is changed and thus influencing the axial velocity distributions. The inlet flow field varies mainly due to the combined effect of the radial pressure gradient and the CF component. The axial velocity varies consistently with the incidence variation induced by the sweep, as observed in the previous literature. In addition, factors that might influence the radial equilibrium such as blade camber angles, solidity and the effect of the distance from the leading edge are also taken into consideration and comparatively analyzed.     

Weighted marginal fisher analysis with spatially smooth for aircraft recognition

Due to limitations to extract invariant features for recognition when the aircraft presents various poses and lacks enough samples for training, a novel algorithm called Weighted Marginal Fisher Analysis with Spatially Smooth （WMFA-SS） for extracting invariant features in aircraft rec- ognition is proposed. According to the Graph Embedding （GE） framework, Heat Kernel function is firstly introduced to characterize the interclass separability when choosing the weights of penalty graph. Furthermore, Laplacian penalty is applied to constraining the coefficients to be spatially smooth in this algorithm. Laplacian penalty is able to incorporate the prior information that neigh- boring pixels are correlated. Besides, using a Laplacian penalty can also avoid the singularity of Laplacian matrix of intrinsic graph. Once compact representations of the images are obtained, it can be considered as invariant features and then be performed in classification to recognize different patterns of aircraft. Real aircraft recognition experiments show the superiority of our proposed WMFA-SS in comparison to other GE algorithms and the current aircraft recognition algorithm; the accuracy rate of our proposed method is 90.00% for dataset BH-AIR1.0 and 99.25% for dataset BH-AIR2.0.     

Comparison of AC drives for electric vehicles-a report on experts'opinion survey

It is recognized that wide applications of electric vehicles (EVs) will bring tremendous social, economical and ecological benefits. With the growing interests in electric vehicles, much effort is demanded for the development of efficient, reliable and economical AC drives' for EV propulsion purpose. Both induction motor (IM) drives and permanent magnet brushless DC motor (IM) drives have been applied to EVs. Switched reluctance motor (SRM) drives have been proposed as an alternative for EV propulsion. In order to assess the suitability of IM, BDCM and SRM drives for EV applications and to provide a technical support for the development and selection of future EV propulsion systems, the existing EV AC propulsion drives were compared, and a survey of experts' opinions was conducted. Comparison of the three AC drives was made on a relative and a quantitative basis using the survey questionnaires. According to the majority of the experts, induction motor drives are best suited for EV propulsion purpose, due to their low cost, high reliability, high speed, established converter and manufacturing technology, low torque ripple/noise and absence of position sensors. BDCM drives feature compactness, low weight and high efficiency and therefore provide an alternative for EV propulsion. The experts regard insulated gate bipolar transistors (IGBTs) as the most suited power semiconductor devices for AC drive converters at the present stage     

平台防飞软件的设计依据

本文叙述了在导弹控制系统试验中因平台倒台而造成飞转的基本原理，为了控制国平台飞转而造成的故障损失，提出建立平台防飞软件的设计依据。     

新型防空导弹制导控制系统展望

本文从防空导弹面临的新挑战出发,对新型防空导弹制导控制系统的技术发展进行了展望。提出了15项应该发展的制导控制技术以期引起读者的兴趣。     

Decoupling and tracking control of induction motor drive

This work introduces an adaptive observation system and a robust control system for achieving the favorable decoupling control and high-precision speed tracking property of an induction motor (IM) drive system. First, an adaptive observation system with an inverse rotor time-constant observer is derived on the basis of model reference adaptive system (MRAS) theory to preserve the decoupling control characteristic of an indirect field-oriented IM drive. The adaptive observation system is implemented using a digital signal processor (DSP) with a high sampling rate to make it possible to achieve good dynamics. Moreover, a robust control system is developed based on the principle of computed torque control. In the robust control system, a grey uncertainty predictor is utilized to adapt the lumped uncertainty on line to relax the requirement of the lumped uncertainty in the design of a computed torque speed controller. In addition, the effectiveness of the proposed observation and control systems is verified by simulated and experimental results.     

飞机横向敏捷性的优化计算

讨论了横向敏捷性指标——飞机带过载情况下滚转并捕获 90°滚转角的时间的计算评估问题。由于该指标值对操纵输入规律的变化较敏感 ,使不同飞机间敏捷性评估缺乏可比性。为了消除驾驶技术对其的影响 ,提出了最优横向敏捷性指标的概念 ,并建立了用遗传算法计算最优横向敏捷性的模型 ,通过选取适当的适应度函数及遗传操作算子 ,对最优横向敏捷性进行了计算。仿真结果表明 ,该优化方法在横向敏捷性计算评估中 ,具有良好的工程性和鲁棒性     

复合材料包装箱的研制与应用

文章对某复合材料包装箱的研制进行了重点介绍。     

Future fighter fable: a day in the life of a future fighter-how dowe get there from here?

The intent of this tongue-in-cheek paper is to stimulate thought about technologies that may be included in future weapons systems and how the weapon system developer is impacted today. It explores a day in the life of a future generation fighter aircraft (year 2015-2025 time-frame). The scenario starts from the perspective of the ground crew awaiting the return of their future fighters: the new A/F-2, “Thunderchief II”-to a dispersed operations location (DOL) from a combat air patrol (CAP) mission in the fictitious country of Crad. A nonrestrictive technology view is assumed, tempered with as much realism as one can logically include in the scenario, with some of today's evolving technology thrusts