亚洲免费人人妻人人,cao78在线视频,福建一级毛片,91精品视频免费观看,高清另类图片操逼,日本特黄特色大片免费看,超碰欧美人人澡曰曰澡夜夜泛

Satellite Constellation Design with

時(shí)間:2023-04-30 01:03:33 航空航天論文 我要投稿
  • 相關(guān)推薦

Satellite Constellation Design with Adaptively Continuous Ant System Algorithm

The ant system algorithm (ASA) has proved to be a novel meta-heuristic algorithm to solve many multivariable problems. In this paper, the earth coverage of satellite constellation is analyzed and a (n + 1)-fold coverage rate is put forward to evaluate the coverage performance of a satellite constellation. An optimization model of constellation parameters is established on the basis of the coverage performance. As a newly developed method, ASA can be applied to optimize the constellation parameters. In order to improve the ASA,a rule for adaptive number of ants is proposed, by which the search range is obviously enlarged and the convergence speed increased.Simulation results have shown that the ASA is more quick and efficient than other methods.

作 者: He Quan Han Chao   作者單位: School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China  刊 名: 中國航空學(xué)報(bào)(英文版)  ISTIC 英文刊名: CHINESE JOURNAL OF AERONAUTICS  年,卷(期): 2007 20(4)  分類號(hào): V2  關(guān)鍵詞: ant system algorithm   satellite constellation   optimization design   coverage performance   adaptive adjusting  

【Satellite Constellation Design with 】相關(guān)文章:

Knowledge Fusion Design Method: Satellite Module Layout04-26

Chinas Meteorological Satellite Application System04-26

Change-1 Satellite Completed Its Preset Objectives04-27

Optimum municipal wastewater treatment plant design with consideration of uncertainty04-26

英文求職信-Design / Creative - Production Artist04-26

Ivar asteroid rendezvous mission system scenario and trajectory design04-26

英文求職信-Design / Creative - Senior Graphic Designer04-26

Chuangxin-1-02 And Shiyan Satellite 3 Launched Atop A LM-2D04-27

A Quasi-equipotential Field Simulation for Preform Design of P/M Superalloy Disk04-26

Design of Neural Network Variable Structure Reentry Control System for Reusable Launch Vehicle04-26