排序方式: 共有26条查询结果,搜索用时 15 毫秒
21.
基于基因算法与博弈论的气动高升力优化 总被引:3,自引:0,他引:3
A multi-objective evolutionary optimization method (combining genetic algorithms(GAs)and game theory(GT))is presented for high lift multi-airfoil systems in aerospace engineering.Due to large dimension global op-timization problems and the increasing importance of low cost distributed parallel environments,it is a natural idea to replace a globar optimization by decentralized local sub-optimizations using GT which introduces the notion of games associated to an optimization problem.The GT/GAs combined optimization method is used for recon-struction and optimization problems by high lift multi-air-foil desing.Numerical results are favorably compared with single global GAs.The method shows teh promising robustness and efficient parallel properties of coupled GAs with different game scenarios for future advanced multi-disciplinary aerospace techmologies. 相似文献
22.
The Jupiter Energetic Particle Detector Instrument (JEDI) Investigation for the Juno Mission 总被引:1,自引:0,他引:1
B. H. Mauk D. K. Haggerty S. E. Jaskulek C. E. Schlemm L. E. Brown S. A. Cooper R. S. Gurnee C. M. Hammock J. R. Hayes G. C. Ho J. C. Hutcheson A. D. Jacques S. Kerem C. K. Kim D. G. Mitchell K. S. Nelson C. P. Paranicas N. Paschalidis E. Rossano M. R. Stokes 《Space Science Reviews》2017,213(1-4):289-346
The Jupiter Energetic Particle Detector Instruments (JEDI) on the Juno Jupiter polar-orbiting, atmosphere-skimming, mission to Jupiter will coordinate with the several other space physics instruments on the Juno spacecraft to characterize and understand the space environment of Jupiter’s polar regions, and specifically to understand the generation of Jupiter’s powerful aurora. JEDI comprises 3 nearly-identical instruments and measures at minimum the energy, angle, and ion composition distributions of ions with energies from H:20 keV and O: 50 keV to >1 MeV, and the energy and angle distribution of electrons from <40 to >500 keV. Each JEDI instrument uses microchannel plates (MCP) and thin foils to measure the times of flight (TOF) of incoming ions and the pulse height associated with the interaction of ions with the foils, and it uses solid state detectors (SSD’s) to measure the total energy (E) of both the ions and the electrons. The MCP anodes and the SSD arrays are configured to determine the directions of arrivals of the incoming charged particles. The instruments also use fast triple coincidence and optimum shielding to suppress penetrating background radiation and incoming UV foreground. Here we describe the science objectives of JEDI, the science and measurement requirements, the challenges that the JEDI team had in meeting these requirements, the design and operation of the JEDI instruments, their calibrated performances, the JEDI inflight and ground operations, and the initial measurements of the JEDI instruments in interplanetary space following the Juno launch on 5 August 2011. Juno will begin its prime science operations, comprising 32 orbits with dimensions 1.1×40 RJ, in mid-2016. 相似文献
23.
B. H. Mauk J. B. Blake D. N. Baker J. H. Clemmons G. D. Reeves H. E. Spence S. E. Jaskulek C. E. Schlemm L. E. Brown S. A. Cooper J. V. Craft J. F. Fennell R. S. Gurnee C. M. Hammock J. R. Hayes P. A. Hill G. C. Ho J. C. Hutcheson A. D. Jacques S. Kerem D. G. Mitchell K. S. Nelson N. P. Paschalidis E. Rossano M. R. Stokes J. H. Westlake 《Space Science Reviews》2016,199(1-4):471-514
24.
Dorey Jacques Compard Didier 《IEEE transactions on aerospace and electronic systems》1967,(2):259-268
The nitrogen flow characteristics around models is studied with a view to obtaining data which determine the physical state of the plasma. Among all possible techniques, the most adaptable to the special hot-shot conditions?electrostatic probes and VHF microwave reflectometry?is chosen. The experimental apparatus and results in nitrogen are described. The ionization is not homogenous during the shot; this result seems to confirm the assumption that the plasma flow is utilizable only after a delay of more than ten milliseconds following the shock formation period. The hot-shot utilization range is examined for this type of experiment. 相似文献
25.
Jacques Villain 《Space Policy》1996,12(2):129-134
The Baikonur launch site was the world's first and remains its most important in terms of the historic missions that have taken off from it. This article describes the background to the construction of Baikonur, the steps taken to keep it secret from the West, and its chief facilities. It enumerates the major space missions that took place there, as well as acknowledging its failures, e.g. the lunar programmes, before speculating on its future. An increasing emphasis on commercial launches seems likely. 相似文献
26.
A six-component force-measuring balance for impulse wind tunnels is described. The application of semiconductors for force and acceleration measurement, and their mechanical and electronic coupling for the desired operational outputs are given. The dynamic calibration procedures are explained and verified for the conditions encountered in hot-shot-type wind tunnels. 相似文献