語系:
繁體中文
English
說明(常見問題)
回圖書館首頁
手機版館藏查詢
登入
回首頁
到查詢結果
[ author_sort:"hu, qinglei." ]
切換:
標籤
|
MARC模式
|
ISBD
Control allocation for spacecraft un...
~
Hu, Qinglei.
FindBook
Google Book
Amazon
博客來
Control allocation for spacecraft under actuator faults
紀錄類型:
書目-電子資源 : Monograph/item
正題名/作者:
Control allocation for spacecraft under actuator faults/ by Qinglei Hu ... [et al.].
其他作者:
Hu, Qinglei.
出版者:
Singapore :Springer Singapore : : 2021.,
面頁冊數:
xviii, 221 p. :ill., digital ;24 cm.
內容註:
Introduction -- Spacecraft Model and Control Allocation Formulation -- Null-space based Optimal Control Allocation for Spacecraft Stabilization -- Robust finite-time control allocation under actuator misalignment -- Finite-Time Fault-Tolerant Spacecraft Attitude Control and Control allocation with Torque Saturation -- Fault Tolerant Control Allocation of Spacecraft Using Fault Detection and Diagnosis -- Extended State Observer based Optimal Control Allocation -- Nonlinear Proportional-Derivative Control Incorporating Closed-loop Control Allocation -- Closed-Loop-Based Control Allocation for Spacecraft Attitude Stabilization with Actuator Fault -- Conclusion.
Contained By:
Springer Nature eBook
標題:
Actuators. -
電子資源:
https://doi.org/10.1007/978-981-16-0439-3
ISBN:
9789811604393
Control allocation for spacecraft under actuator faults
Control allocation for spacecraft under actuator faults
[electronic resource] /by Qinglei Hu ... [et al.]. - Singapore :Springer Singapore :2021. - xviii, 221 p. :ill., digital ;24 cm.
Introduction -- Spacecraft Model and Control Allocation Formulation -- Null-space based Optimal Control Allocation for Spacecraft Stabilization -- Robust finite-time control allocation under actuator misalignment -- Finite-Time Fault-Tolerant Spacecraft Attitude Control and Control allocation with Torque Saturation -- Fault Tolerant Control Allocation of Spacecraft Using Fault Detection and Diagnosis -- Extended State Observer based Optimal Control Allocation -- Nonlinear Proportional-Derivative Control Incorporating Closed-loop Control Allocation -- Closed-Loop-Based Control Allocation for Spacecraft Attitude Stabilization with Actuator Fault -- Conclusion.
This book provides a systematical and comprehensive description of some facets of modeling, designing, analyzing and exploring the control allocation and fault-tolerant control problems for over-actuated spacecraft attitude control system under actuator failures, system uncertainties and disturbances. The book intends to provide a unified platform for understanding and applicability of the fault-tolerant attitude control and control allocation for different purposes in aerospace engineering and some related fields. And it is particularly suited for readers who are interested to learn solutions in spacecraft attitude control system design and related engineering applications.
ISBN: 9789811604393
Standard No.: 10.1007/978-981-16-0439-3doiSubjects--Topical Terms:
649246
Actuators.
LC Class. No.: TL3260
Dewey Class. No.: 629.4742
Control allocation for spacecraft under actuator faults
LDR
:02379nmm a2200337 a 4500
001
2239180
003
DE-He213
005
20210713113555.0
006
m d
007
cr nn 008maaau
008
211111s2021 si s 0 eng d
020
$a
9789811604393
$q
(electronic bk.)
020
$a
9789811604386
$q
(paper)
024
7
$a
10.1007/978-981-16-0439-3
$2
doi
035
$a
978-981-16-0439-3
040
$a
GP
$c
GP
041
0
$a
eng
050
4
$a
TL3260
072
7
$a
TJFM
$2
bicssc
072
7
$a
TEC004000
$2
bisacsh
072
7
$a
TJFM
$2
thema
072
7
$a
TJFD
$2
thema
082
0 4
$a
629.4742
$2
23
090
$a
TL3260
$b
.C764 2021
245
0 0
$a
Control allocation for spacecraft under actuator faults
$h
[electronic resource] /
$c
by Qinglei Hu ... [et al.].
260
$a
Singapore :
$b
Springer Singapore :
$b
Imprint: Springer,
$c
2021.
300
$a
xviii, 221 p. :
$b
ill., digital ;
$c
24 cm.
505
0
$a
Introduction -- Spacecraft Model and Control Allocation Formulation -- Null-space based Optimal Control Allocation for Spacecraft Stabilization -- Robust finite-time control allocation under actuator misalignment -- Finite-Time Fault-Tolerant Spacecraft Attitude Control and Control allocation with Torque Saturation -- Fault Tolerant Control Allocation of Spacecraft Using Fault Detection and Diagnosis -- Extended State Observer based Optimal Control Allocation -- Nonlinear Proportional-Derivative Control Incorporating Closed-loop Control Allocation -- Closed-Loop-Based Control Allocation for Spacecraft Attitude Stabilization with Actuator Fault -- Conclusion.
520
$a
This book provides a systematical and comprehensive description of some facets of modeling, designing, analyzing and exploring the control allocation and fault-tolerant control problems for over-actuated spacecraft attitude control system under actuator failures, system uncertainties and disturbances. The book intends to provide a unified platform for understanding and applicability of the fault-tolerant attitude control and control allocation for different purposes in aerospace engineering and some related fields. And it is particularly suited for readers who are interested to learn solutions in spacecraft attitude control system design and related engineering applications.
650
0
$a
Actuators.
$3
649246
650
0
$a
Space vehicles
$x
Attitude control systems.
$3
2068355
650
1 4
$a
Control, Robotics, Mechatronics.
$3
1002220
650
2 4
$a
Aerospace Technology and Astronautics.
$3
928116
700
1
$a
Hu, Qinglei.
$3
3492965
710
2
$a
SpringerLink (Online service)
$3
836513
773
0
$t
Springer Nature eBook
856
4 0
$u
https://doi.org/10.1007/978-981-16-0439-3
950
$a
Intelligent Technologies and Robotics (SpringerNature-42732)
筆 0 讀者評論
館藏地:
全部
電子資源
出版年:
卷號:
館藏
1 筆 • 頁數 1 •
1
條碼號
典藏地名稱
館藏流通類別
資料類型
索書號
使用類型
借閱狀態
預約狀態
備註欄
附件
W9401065
電子資源
11.線上閱覽_V
電子書
EB TL3260
一般使用(Normal)
在架
0
1 筆 • 頁數 1 •
1
多媒體
評論
新增評論
分享你的心得
Export
取書館
處理中
...
變更密碼
登入