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
娄底市| 平昌县| 普陀区| 博客| 南丹县| 石家庄市| 定陶县| 蒙山县| 若尔盖县| 徐州市| 淳安县| 正蓝旗| 阿城市| 城市| 禄丰县| 宣城市| 博乐市| 元朗区| 石屏县| 湖口县| 曲靖市| 邳州市| 梁平县| 瓮安县| 辉南县| 南宁市| 长海县| 阳春市| 蒙自县| 五大连池市| 广平县| 内乡县| 嘉义市| 永清县| 阜宁县| 民权县| 郑州市| 颍上县| 高邮市| 辽宁省| 绥中县|