找回密码
 To register

QQ登录

只需一步,快速开始

扫一扫,访问微社区

Titlebook: Smart Small Satellites: Design, Modelling and Development; Proceedings of the I Chander Prakash,V. Sambasiva Rao,D. V. A. Raghava Conferen

[复制链接]
楼主: Perforation
发表于 2025-3-28 17:18:42 | 显示全部楼层
发表于 2025-3-28 19:28:03 | 显示全部楼层
发表于 2025-3-28 23:03:19 | 显示全部楼层
EO Characterization of SATURN SWIR Detector Array,curate determination of, EO parameters of detector array, optical system transfer function and their dependence on thermal and vibration variations. This paper presents the methodology and experimental setup for characterization of the EO parameters for SATURN SWIR integrated detector array and Dewa
发表于 2025-3-29 04:47:55 | 显示全部楼层
发表于 2025-3-29 08:23:22 | 显示全部楼层
,Design and Implementation of 32 W Dual Output Forward Converter with Bias Feedback for Spaceborne Snd coupled inductor for better load and cross regulations were used. This converter will operate at 500 kHz switching frequency and uses UC2825 PWM controller which can operate both in voltage and current mode control. PWM controller has better soft start, maximum control on duty, under voltage and
发表于 2025-3-29 11:56:59 | 显示全部楼层
Design and Implementation of High Frequency Single Output Forward Converter for Space Application,imparting perfect isolation between the input and output. The proposed converter is designed using single switch forward converter topology operating at 500 kHz. A continuous and regulated output of 5 V/8 A is generated from an input range of 18–50 V using voltage mode control through magnetic isola
发表于 2025-3-29 17:31:43 | 显示全部楼层
发表于 2025-3-29 19:53:45 | 显示全部楼层
EMI Reduction of Forward Converter with Backshells and Copper Braid for Space Application,e (EMI) is the possible interference to other electronic equipment. Due to the EMI system performance may effect, to take that need to design the proper EMI filter design and proper harness. Electronic Magnetic Compatibility (EMC) is defined as the ability of devices and systems to operate in their
发表于 2025-3-30 02:23:39 | 显示全部楼层
Solar Panel Deployment Mechanism for Nano-Satellite,nd optimization in terms of mass and volume. The modular hinge mechanism simplifies ground testing and can be operated in Earth’s gravity, thereby eliminating the need for gravity compensation system for solar panel deployment. The miniature hinge is configured without locking linkages and holds the
发表于 2025-3-30 07:02:58 | 显示全部楼层
 关于派博传思  派博传思旗下网站  友情链接
派博传思介绍 公司地理位置 论文服务流程 影响因子官网 SITEMAP 大讲堂 北京大学 Oxford Uni. Harvard Uni.
发展历史沿革 期刊点评 投稿经验总结 SCIENCEGARD IMPACTFACTOR 派博系数 清华大学 Yale Uni. Stanford Uni.
|Archiver|手机版|小黑屋| 派博传思国际 ( 京公网安备110108008328) GMT+8, 2025-5-21 16:41
Copyright © 2001-2015 派博传思   京公网安备110108008328 版权所有 All rights reserved
快速回复 返回顶部 返回列表