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標(biāo)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 [打印本頁]

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作者: 著名    時間: 2025-3-21 21:25
Control Allocation for Spacecraft Under Actuator Faults978-981-16-0439-3
作者: indemnify    時間: 2025-3-22 03:06

作者: 果仁    時間: 2025-3-22 06:05

作者: 極肥胖    時間: 2025-3-22 12:04
Nonlinear Proportional-Derivative Control Incorporating Closed-Loop Control Allocation for Spacecraiscrepancies or saturation phenomenon may reduce the control system performances and even cause the instability of the whole control system if it could be well handled and solved. All of the above mentioned problems cause considerable difficulties and challenges in the spacecraft ACS design, for mee
作者: 胰島素    時間: 2025-3-22 16:46
Closed-Loop Based Control Allocation for Spacecraft Attitude Stabilization with Actuator Faults,ve SMC law to dynamically compensate the perturbations due to actuator faults and other uncertainties, in which the real time CA algorithm delivers the control command to actuators. In [.], a novel dynamic near-optimal CA scheme with combination of a saturated baseline controller for spacecraft atti
作者: 胰島素    時間: 2025-3-22 20:02

作者: 外來    時間: 2025-3-22 21:19
Closed-Loop Based Control Allocation for Spacecraft Attitude Stabilization with Actuator Faults,be degraded, even the unstable ACS may result in the completely collapse, immeasurable losses or catastrophic consequences. Thus, the spacecraft ACS should be capable of dealing with or tolerating possible actuator faults, while at the same time guaranteeing an acceptable performance in the presence
作者: BOOR    時間: 2025-3-23 03:01
Qinglei Hu,Bo Li,Youmin ZhangPresents the existing and emerging concepts concerning control allocation, and attitude control and fault-tolerant control for the over-actuated spacecraft under actuator failures.Addresses the resear
作者: 領(lǐng)帶    時間: 2025-3-23 09:07
http://image.papertrans.cn/c/image/237226.jpg
作者: collateral    時間: 2025-3-23 13:30
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.
作者: 雄辯    時間: 2025-3-23 17:21
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.
作者: Eulogy    時間: 2025-3-23 20:55
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.
作者: HERTZ    時間: 2025-3-24 02:02

作者: 運(yùn)動的我    時間: 2025-3-24 04:08
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.
作者: BILK    時間: 2025-3-24 09:38
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.
作者: 逃避系列單詞    時間: 2025-3-24 13:22
Edoardo Del Pezzo,Domenico PatanéFor the over-actuated spacecraft ACS, it is generally equipped with redundant actuators in the specified configurations.
作者: 誘拐    時間: 2025-3-24 16:41

作者: 擦掉    時間: 2025-3-24 19:42
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.
作者: GEN    時間: 2025-3-25 00:08
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.
作者: 欺騙世家    時間: 2025-3-25 06:09
Null-Space Based Optimal Control Allocation for Spacecraft Attitude Stabilization,For 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.
作者: Diaphragm    時間: 2025-3-25 07:36
Robust Finite-Time Control Allocation for Attitude Stabilization Under Actuator Misalignment,Attitude control of a rigid spacecraft has attracted tremendous attention for the capability of achieving operational services, such as remote sensing, communication and variety of space-related research.
作者: 欄桿    時間: 2025-3-25 14:14
Finite-Time Fault-Tolerant Spacecraft Attitude Control with Torque Saturation,On-orbiting spacecraft are working for a specified long time under the effects of environmental disturbances, uncertainties, component failures, and input saturation.
作者: 礦石    時間: 2025-3-25 17:51
Extended State Observer Based Optimal Attitude Robust Control of Spacecraft,In practical applications, the external disturbances and uncertainties are always exist for the spacecraft attitude control system.
作者: Functional    時間: 2025-3-25 23:28

作者: apropos    時間: 2025-3-26 01:32
Conclusions,For on-orbiting spacecraft, FTC and CA techniques are generally utilized to ensure the stability, reliability, autonomy and intelligence, and the percentage of successfully accomplished missions of the spacecraft ACS, especially in the presence of external disturbances, actuator constraints and faults.
作者: Forehead-Lift    時間: 2025-3-26 04:23
https://doi.org/10.1007/978-981-16-0439-3Spacecraft; Attitude Control; Control Allocation; Fault Tolerant Control; Finite-Time Control; Actuator F
作者: 變化    時間: 2025-3-26 08:48

作者: 亂砍    時間: 2025-3-26 14:14
IAVCEI Proceedings in Volcanologycecraft ACS design. For orbiting spacecraft, dynamics are strongly nonlinear in nature and are also affected by various external disturbances from the environment that influence the mission objectives significantly. In addition, actuator uncertainties induced by misalignment during installation and
作者: limber    時間: 2025-3-26 19:35

作者: 原始    時間: 2025-3-26 21:54
he?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.?978-981-16-0441-6978-981-16-0439-3
作者: Fortify    時間: 2025-3-27 02:29
ated spacecraft under actuator failures.Addresses the researThis 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 u
作者: 整潔漂亮    時間: 2025-3-27 09:02

作者: 同位素    時間: 2025-3-27 09:27

作者: 無瑕疵    時間: 2025-3-27 13:59

作者: SHOCK    時間: 2025-3-27 20:49

作者: Infinitesimal    時間: 2025-3-27 23:20
,Biaxial Compressive Strength of Silicon Nitride: New Data — Micromechanics Models,e stress except possibly close to the equi-biaxial compressive state. It was found in another study that, in contrast to alumina and siliconized silicon carbide, the compressive failure of silicon nitride is not induced by the growth of cracks from Griffith flaws. Tests were conducted to discover wh
作者: Critical    時間: 2025-3-28 02:47

作者: AVANT    時間: 2025-3-28 06:37
Clinical Approach to the Diagnosis of Autoinflammatory Diseasestory, physical examination, system involvement and laboratory testing and offer an algorithm on investigative pathways for these patients. We discuss the various diagnostic criteria currently used for specific autoinflammatory diseases. Finally, we propose an approach, including empiric treatment an
作者: 整潔漂亮    時間: 2025-3-28 11:33

作者: synovium    時間: 2025-3-28 16:14

作者: 凈禮    時間: 2025-3-28 20:33
https://doi.org/10.1007/978-3-8349-9070-9le by any other state-of-the-art techniques, including . and ., within 8?h. We also identify a bug (reports safe instead of unsafe) and 48 counterexample generation errors in the tools compared in our analysis.
作者: 統(tǒng)治人類    時間: 2025-3-28 22:59

作者: Pantry    時間: 2025-3-29 04:46

作者: CHANT    時間: 2025-3-29 08:04
ance and what is more it is great fun. Many of the diagrams have been retained, but some have been redrawn and new ones added. Weare pleased to acknowledge the patience and artistic skills of Mrs Lindsay J. Wilson in producing these. Some coloured plates have also been introduced from photographs ta
作者: abstemious    時間: 2025-3-29 14:14
Textbook 2008Latest editionughout his life he was inspired by geometry and poetry, and favored elegant succinct proofs. This little book, ?rst published in 1944,then in a secondexpanded edition in 1987, gives us a glimpse into his way of thinking. It is a series of vignettes, each crafted with elegance and economy. See, for e
作者: growth-factor    時間: 2025-3-29 17:42

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