找回密碼
 To register

QQ登錄

只需一步,快速開始

掃一掃,訪問微社區(qū)

打印 上一主題 下一主題

Titlebook: Control Allocation for Spacecraft Under Actuator Faults; Qinglei Hu,Bo Li,Youmin Zhang Book 2021 The Editor(s) (if applicable) and The Aut

[復(fù)制鏈接]
樓主: commingle
11#
發(fā)表于 2025-3-23 13:30:21 | 只看該作者
Visualisierung von VolumendatenThe exploration of deep space is of great significance and promotion for the human development and technological progress. It has been extensively and will be continuously supported by the USA, Europe, Russia and China, etc.
12#
發(fā)表于 2025-3-23 17:21:58 | 只看該作者
Visualisierung von VolumendatenThis chapter gives a brief introduction to the attitude kinematics and dynamics of a rigid spacecraft, as well as some related basic knowledge.
13#
發(fā)表于 2025-3-23 20:55:17 | 只看該作者
Andreas Winklhofer,Gerhard K?stlerFor the on-orbiting spacecraft, the accurate and reliable ACS is very important and necessary for the accomplishment of the aerospace missions, such as attitude stabilization, high-precision pointing, attitude tracking or maneuver.
14#
發(fā)表于 2025-3-24 02:02:01 | 只看該作者
15#
發(fā)表于 2025-3-24 04:08:16 | 只看該作者
State of the Art in Volcanic SeismologyOn-orbiting spacecraft are working for a specified long time under the effects of environmental disturbances, uncertainties, component failures, and input saturation.
16#
發(fā)表于 2025-3-24 09:38:18 | 只看該作者
S. A. Fedotov,V. I. Gorelchik,N. A. ZharinovIn practical applications, the external disturbances and uncertainties are always exist for the spacecraft attitude control system.
17#
發(fā)表于 2025-3-24 13:22:49 | 只看該作者
Edoardo Del Pezzo,Domenico PatanéFor the over-actuated spacecraft ACS, it is generally equipped with redundant actuators in the specified configurations.
18#
發(fā)表于 2025-3-24 16:41:47 | 只看該作者
19#
發(fā)表于 2025-3-24 19:42:00 | 只看該作者
Introduction,The exploration of deep space is of great significance and promotion for the human development and technological progress. It has been extensively and will be continuously supported by the USA, Europe, Russia and China, etc.
20#
發(fā)表于 2025-3-25 00:08:46 | 只看該作者
Mathematical Model of the Attitude Control System,This chapter gives a brief introduction to the attitude kinematics and dynamics of a rigid spacecraft, as well as some related basic knowledge.
 關(guān)于派博傳思  派博傳思旗下網(wǎng)站  友情鏈接
派博傳思介紹 公司地理位置 論文服務(wù)流程 影響因子官網(wǎng) 吾愛論文網(wǎng) 大講堂 北京大學(xué) Oxford Uni. Harvard Uni.
發(fā)展歷史沿革 期刊點評 投稿經(jīng)驗總結(jié) SCIENCEGARD IMPACTFACTOR 派博系數(shù) 清華大學(xué) Yale Uni. Stanford Uni.
QQ|Archiver|手機(jī)版|小黑屋| 派博傳思國際 ( 京公網(wǎng)安備110108008328) GMT+8, 2025-10-12 20:33
Copyright © 2001-2015 派博傳思   京公網(wǎng)安備110108008328 版權(quán)所有 All rights reserved
快速回復(fù) 返回頂部 返回列表
通辽市| 营山县| 弥勒县| 视频| 宝山区| 弥渡县| 新乡市| 博罗县| 鹤峰县| 九台市| 普陀区| 苍梧县| 闸北区| 洪雅县| 白沙| 张掖市| 资溪县| 新平| 黄冈市| 威信县| 临洮县| 涟水县| 米林县| 永年县| 荆州市| 错那县| 时尚| 集贤县| 陆川县| 革吉县| 澎湖县| 乌兰浩特市| 阳城县| 商丘市| 鄂州市| 寻乌县| 衡阳县| 乐平市| 商水县| 新蔡县| 桐庐县|