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311.
北京大学低速风洞中采用一种新的测量侧滑振动导数的原理和技术,它利用同一强迫振动装置,更换少许运动转换件和支杆,实现五种单自由度强迫振动,由六分量天平和相关滤波仪器测量出全部组合导数和下洗时差导数,而侧滑振动导数是通过对应的侧滑-滚转振动与演转振动测出的组合导数之差得到的。本文给出了某教练机大攻角侧洗时差导数的典型结果。 相似文献
312.
Optimization problems are often highly constrained and evolutionary algorithms(EAs)are effective methods to tackle this kind of problems. To further improve search efficiency and convergence rate of EAs, this paper presents an adaptive double chain quantum genetic algorithm(ADCQGA) for solving constrained optimization problems. ADCQGA makes use of doubleindividuals to represent solutions that are classified as feasible and infeasible solutions. Fitness(or evaluation) functions are defined for both types of solutions. Based on the fitness function, three types of step evolution(SE) are defined and utilized for judging evolutionary individuals. An adaptive rotation is proposed and used to facilitate updating individuals in different solutions.To further improve the search capability and convergence rate, ADCQGA utilizes an adaptive evolution process(AEP), adaptive mutation and replacement techniques. ADCQGA was first tested on a widely used benchmark function to illustrate the relationship between initial parameter values and the convergence rate/search capability. Then the proposed ADCQGA is successfully applied to solve other twelve benchmark functions and five well-known constrained engineering design problems. Multi-aircraft cooperative target allocation problem is a typical constrained optimization problem and requires efficient methods to tackle. Finally, ADCQGA is successfully applied to solving the target allocation problem. 相似文献
313.
Bruno Mialon Alex Khrabrov Saloua Ben Khelil Andreas Huebner Andrea Da Ronch Ken Badcock Luca Cavagna Peter Eliasson Mengmeng Zhang Sergio Ricci Jean-Christophe Jouhaud Gilbert Rogé Stephan Hitzel Martin Lahuta 《Progress in Aerospace Sciences》2011,47(8):674-694
The dynamic derivatives are widely used in linear aerodynamic models in order to determine the flying qualities of an aircraft: the ability to predict them reliably, quickly and sufficiently early in the design process is vital in order to avoid late and costly component redesigns. This paper describes experimental and computational research dealing with the determination of dynamic derivatives carried out within the FP6 European project SimSAC. Numerical and experimental results are compared for two aircraft configurations: a generic civil transport aircraft, wing-fuselage-tail configuration called the DLR-F12 and a generic Transonic CRuiser, which is a canard configuration. Static and dynamic wind tunnel tests have been carried out for both configurations and are briefly described within this paper. The data generated for both the DLR-F12 and TCR configurations include force and pressure coefficients obtained during small amplitude pitch, roll and yaw oscillations while the data for the TCR configuration also include large amplitude oscillations, in order to investigate the dynamic effects on nonlinear aerodynamic characteristics. In addition, dynamic derivatives have been determined for both configurations with a large panel of tools, from linear aerodynamic (Vortex Lattice Methods) to CFD. This work confirms that an increase in fidelity level enables the dynamic derivatives to be calculated more accurately. Linear aerodynamics tools are shown to give satisfactory results but are very sensitive to the geometry/mesh input data. Although all the quasi-steady CFD approaches give comparable results (robustness) for steady dynamic derivatives, they do not allow the prediction of unsteady components for the dynamic derivatives (angular derivatives with respect to time): this can be done with either a fully unsteady approach i.e. with a time-marching scheme or with frequency domain solvers, both of which provide comparable results for the DLR-F12 test case. As far as the canard configuration is concerned, strong limitations for the linear aerodynamic tools are observed. A key aspect of this work are the acceleration techniques developed for CFD methods, which allow the computational time to be dramatically reduced while providing comparable results. 相似文献
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Recently, asteroid exploration becomes an important branch of human’s deep space activities. In this paper, a piecewise linear optimal orbital maneuver strategy is designed for a spacecraft soft landing on irregular-shaped asteroids. First, the space around an irregular asteroid is converted into several grid units, and the gravitational field of the asteroid is linearly fitted in each unit.Then, the soft-landing orbital maneuver strategy design problem is formulated as a piecewise linear optima... 相似文献
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结合某型飞机的研制 ,总结了歼击机配装主动雷达型导弹需要解决的关键技术 ,论述了解决这些关键技术的一般技术途径和方法。 相似文献
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Stephen Potter 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2006,38(12):2832-2835
I discuss methods and results in the use of photo-polarimetry and spectro-polarimetry in the studies of magnetic cataclysmic variables. In particular I show how polarimetry can be used to derive the geometry of the accretion region on the surface of the white dwarf, the accreting geometry of the system as a whole and how polarimetry aides in the interpretation of X-ray/optical photometry and spectroscopy. I finish by describing the high speed spectro-polarimetric capabilities of SALT (Southern African Large Telescope) due for completion in 2005. 相似文献
320.
大区域中心城市是指具有跨区域作用和意义的中心城市。本文用定量分析的方法,将郑州与周边省会城市的中心度进行了对比分析,从而得出郑州最有可能成为中源地区及至陇兰经济带的核心城市的结论。 相似文献