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Nonsingular Fast Terminal Adaptive Neuro-sliding Mode Control for Spacecraft Formation Flying Systems

Xiaohan Lin, Xiaoping Shi, Shilun Li, Sing Kiong Nguang, Liruo Zhang
<span title="2020-05-30">2020</span> <i title="Hindawi Limited"> <a target="_blank" rel="noopener" href="https://fatcat.wiki/container/y3fh56bfunh5fgneywwba6d4ke" style="color: black;">Complexity</a> </i> &nbsp;
Second, a fast nonsingular terminal sliding mode control law is proposed to guarantee the tracking errors of the spacecraft formation converge to zero in finite time.  ...  The proposed sliding mode control laws not only achieve the formation but also alleviate the effect of the chattering.  ...  Sliding Mode Control Law with Supertwisting Disturbance Observer.  ... 
<span class="external-identifiers"> <a target="_blank" rel="external noopener noreferrer" href="https://doi.org/10.1155/2020/5875191">doi:10.1155/2020/5875191</a> <a target="_blank" rel="external noopener" href="https://fatcat.wiki/release/5bcv7jau7bbhnasri4x6xdjrca">fatcat:5bcv7jau7bbhnasri4x6xdjrca</a> </span>
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Adaptive tracking control for spacecraft formation flying system via modified fast integral terminal sliding mode surface

Xiaohan Lin, Xiaoping Shi, Shilun Li
<span title="">2020</span> <i title="Institute of Electrical and Electronics Engineers (IEEE)"> <a target="_blank" rel="noopener" href="https://fatcat.wiki/container/q7qi7j4ckfac7ehf3mjbso4hne" style="color: black;">IEEE Access</a> </i> &nbsp;
The disturbance estimation ability of the proposed observer (45)-(46) is improved significantly with high accuracy.  ...  NUMERICAL SIMULATION To illustrate the effectiveness and various features of the fast integral terminal sliding mode control law, the control law with reduced-order disturbance observer, and adaptive  ... 
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Adaptive Integral-type Sliding Mode Control for Spacecraft Attitude Maneuvering Under Actuator Stuck Failures

Qinglei HU, Youmin ZHANG, Xing HUO, Bing XIAO
<span title="">2011</span> <i title="Elsevier BV"> <a target="_blank" rel="noopener" href="https://fatcat.wiki/container/7j7rymwfdvdgha64ol5ajggjqa" style="color: black;">Chinese Journal of Aeronautics</a> </i> &nbsp;
Complete stability and performance analysis are presented and illustrative simulation results of application to a spacecraft show that high precise attitude control with zero steady-error is successfully  ...  A fault tolerant control (FTC) design technique against actuator stuck faults is investigated using integral-type sliding mode control (ISMC) with application to spacecraft attitude maneuvering control  ...  Fault Tolerant Attitude Controller Design with Stuck Failures In this section, we present the design procedure to implement adaptive integral sliding mode-based FTC for spacecraft attitude control system  ... 
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Adaptive Fuzzy Sliding-Mode Attitude Controller Design for Spacecrafts with Thrusters [chapter]

Fu-Kuang Yeh
<span title="2012-03-23">2012</span> <i title="InTech"> Advances in Spacecraft Systems and Orbit Determination </i> &nbsp;
, the fuzzy sliding-mode and the adaptive fuzzy sliding-mode attitude controllers.  ...  Adaptive fuzzy sliding-mode attitude controller design Since the sliding-mode attitude controller for a spacecraft requires estimating upper bounds (constant values) of the lumped uncertainty, so that  ...  Adaptive Fuzzy Sliding-Mode Attitude Controller Design for Spacecrafts with Thrusters, Advances in Spacecraft Systems and Orbit Determination, Dr.  ... 
<span class="external-identifiers"> <a target="_blank" rel="external noopener noreferrer" href="https://doi.org/10.5772/38189">doi:10.5772/38189</a> <a target="_blank" rel="external noopener" href="https://fatcat.wiki/release/nah4ih4amrfxzef2psvjp4ynpy">fatcat:nah4ih4amrfxzef2psvjp4ynpy</a> </span>
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Adaptive Fixed-Time Nonsingular Terminal Sliding Mode Attitude Tracking Control for Spacecraft with Actuator Saturations and Faults

Zhiguo Han, Minghao Wang, Xunliang Yan, Hang Qian, Paolo Castaldi
<span title="2021-02-05">2021</span> <i title="Hindawi Limited"> <a target="_blank" rel="noopener" href="https://fatcat.wiki/container/75xpl4z7arculfjaok5ombj2ju" style="color: black;">International Journal of Aerospace Engineering</a> </i> &nbsp;
The designed fixed-time adaptive nonsingular terminal sliding mode control law is applicable to the development of fixed-time fault-tolerant attitude tracking controller with multiple constraints.  ...  Based on the adaptive nonsingular terminal sliding mode control theory, we design a kind of fixed-time convergence control method.  ...  The research is financially supported by the National Natural Science Foundation of China (No. 61502391, 11602296), the Natural Science Foundation of Shaanxi Province (Grant no. 2019JM-434), and Aviation  ... 
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New Developments in Sliding Mode Control and Its Applications 2014

Ligang Wu, Rongni Yang, Guanghui Sun, Xudong Zhao, Peng Shi
<span title="">2015</span> <i title="Hindawi Limited"> <a target="_blank" rel="noopener" href="https://fatcat.wiki/container/wpareqynwbgqdfodcyhh36aqaq" style="color: black;">Mathematical Problems in Engineering</a> </i> &nbsp;
"Finite-Time Reentry Attitude Control Using Time-Varying Sliding Mode and Disturbance Observer" by X.  ...  compensator and a dynamicinversion-based sliding mode controller, while "Unknown Disturbance Estimation for a PMSM with a Hybrid Sliding Mode Observer" by G.  ... 
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Integrated Fault Estimation and Fault-Tolerant Control for Rigid Spacecraft Attitude System with Multiple Actuator Faults

Xiaobo Zhang, Zhifeng Gao, Moshu Qian, Lang Bai
<span title="">2019</span> <i title="ICIC International"> <a target="_blank" rel="noopener" href="https://fatcat.wiki/container/gj6lacbygvhjhbfu4ttj3j645a" style="color: black;">International Journal of Innovative Computing, Information and Control</a> </i> &nbsp;
Firstly, an adaptive sliding mode fault estimation observer is designed for the faulty rigid spacecraft attitude system to get the estimated values of actuator faults under the existence of unknown inertia  ...  Then, an integrated FE/FTC attitude control strategy is developed by using both fractional-order nonsingular terminal sliding mode (FONTSM) method and backstepping technology, and it could guarantee that  ...  Therefore, it is one of the main contributions of the sliding mode fault estimation observer designed in this paper. [24] , the sliding mode fault estimation observer must select too high switching term  ... 
<span class="external-identifiers"> <a target="_blank" rel="external noopener noreferrer" href="https://doi.org/10.24507/ijicic.15.04.1255">doi:10.24507/ijicic.15.04.1255</a> <a target="_blank" rel="external noopener" href="https://fatcat.wiki/release/spdf4foii5fdhpne2avai24i4e">fatcat:spdf4foii5fdhpne2avai24i4e</a> </span>
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Anti-Unwinding Attitude Control with Fixed-Time Convergence for a Flexible Spacecraft

Chutiphon Pukdeboon, Anuchit Jitpattanakul
<span title="">2017</span> <i title="Hindawi Limited"> <a target="_blank" rel="noopener" href="https://fatcat.wiki/container/75xpl4z7arculfjaok5ombj2ju" style="color: black;">International Journal of Aerospace Engineering</a> </i> &nbsp;
This paper investigates the fixed-time attitude tracking control problem for flexible spacecraft with unknown bounded disturbances.  ...  Second, the controller is further enhanced by an adaptive law to avoid the knowledge of norm upper bounds of external disturbances and coupling effect of flexible modes.  ...  Conflicts of Interest The authors declare that there are no conflicts of interest regarding the publication of this paper.  ... 
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New Developments in Sliding Mode Control and Its Applications

Ligang Wu, Rongni Yang, Guanghui Sun, Xudong Zhao, Peng Shi
<span title="">2014</span> <i title="Hindawi Limited"> <a target="_blank" rel="noopener" href="https://fatcat.wiki/container/wpareqynwbgqdfodcyhh36aqaq" style="color: black;">Mathematical Problems in Engineering</a> </i> &nbsp;
An et al. is concerned with the sliding mode observer design framework and a second order geometric sliding mode attitude observer is designed for angular velocity estimation of quadrotor attitude.  ...  "Adaptive backstepping finite time attitude control of reentry RLV with input constraint" by F.  ...  An et al. is concerned with the sliding mode observer design framework and a second order geometric sliding mode attitude observer is designed for angular velocity estimation of quadrotor attitude.  ... 
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Nonsingular Integral Sliding Mode Attitude Control for Rigid-Flexible Coupled Spacecraft with High-Inertia Rotating Appendages

Gaowang Zhang, Xueqin Chen, Ruichen Xi, Huayi Li, Rui Wang
<span title="2021-02-15">2021</span> <i title="Hindawi Limited"> <a target="_blank" rel="noopener" href="https://fatcat.wiki/container/y3fh56bfunh5fgneywwba6d4ke" style="color: black;">Complexity</a> </i> &nbsp;
To address the complex control problem, a novel, fast nonsingular integral sliding mode control method is proposed to perform the attitude tracking function of spacecraft.  ...  This study addresses the challenge of attitude tracking control for a rigid-flexible spacecraft with high-inertia rotating appendages.  ...  In [19] [20] [21] , effective disturbance observers were designed for controlled systems to achieve high performance in the presence of inertia uncertainties and external disturbances.  ... 
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Finite-Time Attitude Stabilization Adaptive Control for Spacecraft with Actuator Dynamics

Wang, Ye, Mu, Sun, Wu
<span title="2019-12-16">2019</span> <i title="MDPI AG"> <a target="_blank" rel="noopener" href="https://fatcat.wiki/container/taedaf6aozg7vitz5dpgkojane" style="color: black;">Sensors</a> </i> &nbsp;
The results show that the high-precision attitude control performance can be achieved by the proposed scheme.  ...  For the attitude stabilization of spacecraft with actuator dynamics, this paper proposed a finite-time control law. Firstly, the dynamic property of the actuator is analyzed by an example.  ...  A controller was proposed using the fast nonsingular terminal sliding mode manifold with a weighted homogeneous extended state observer estimating unknown disturbance.  ... 
<span class="external-identifiers"> <a target="_blank" rel="external noopener noreferrer" href="https://doi.org/10.3390/s19245568">doi:10.3390/s19245568</a> <a target="_blank" rel="external noopener" href="https://www.ncbi.nlm.nih.gov/pubmed/31888307">pmid:31888307</a> <a target="_blank" rel="external noopener" href="https://pubmed.ncbi.nlm.nih.gov/PMC6960679/">pmcid:PMC6960679</a> <a target="_blank" rel="external noopener" href="https://fatcat.wiki/release/nvspvlghqvddbaiedv7jhs3lvm">fatcat:nvspvlghqvddbaiedv7jhs3lvm</a> </span>
<a target="_blank" rel="noopener" href="https://web.archive.org/web/20191218010743/https://res.mdpi.com/d_attachment/sensors/sensors-19-05568/article_deploy/sensors-19-05568.pdf" title="fulltext PDF download" data-goatcounter-click="serp-fulltext" data-goatcounter-title="serp-fulltext"> <button class="ui simple right pointing dropdown compact black labeled icon button serp-button"> <i class="icon ia-icon"></i> Web Archive [PDF] <div class="menu fulltext-thumbnail"> <img src="https://blobs.fatcat.wiki/thumbnail/pdf/96/c2/96c2fc7500506492544dfa69677785eeaa287111.180px.jpg" alt="fulltext thumbnail" loading="lazy"> </div> </button> </a> <a target="_blank" rel="external noopener noreferrer" href="https://doi.org/10.3390/s19245568"> <button class="ui left aligned compact blue labeled icon button serp-button"> <i class="unlock alternate icon" style="background-color: #fb971f;"></i> mdpi.com </button> </a> <a target="_blank" rel="external noopener" href="https://www.ncbi.nlm.nih.gov/pmc/articles/PMC6960679" title="pubmed link"> <button class="ui compact blue labeled icon button serp-button"> <i class="file alternate outline icon"></i> pubmed.gov </button> </a>

Adaptive Sliding Mode Attitude and Vibration Control of Flexible Spacecraft Under Unknown Disturbance and Uncertainty

Qinglei Hu, Michael I. Friswell
<span title="">2008</span> <i title="Elsevier BV"> <a target="_blank" rel="noopener" href="https://fatcat.wiki/container/p3wtlm3j2fedxitkuu4bs3scau" style="color: black;">IFAC Proceedings Volumes</a> </i> &nbsp;
This is followed by the design of an adaptive sliding mode control (ASMC) law using only the output for robust stabilization of spacecraft in the presence of parametric uncertainty and external disturbances  ...  As a stepping stone, a state feedback sliding mode control command is designed for the reaction wheel to achieve the reference trajectory tracking control of attitude angle.  ...  ACKNOWLEDGEMENTS The authors gratefully acknowledge the support of the Program for Young Excellent Talents  ... 
<span class="external-identifiers"> <a target="_blank" rel="external noopener noreferrer" href="https://doi.org/10.3182/20080706-5-kr-1001.01670">doi:10.3182/20080706-5-kr-1001.01670</a> <a target="_blank" rel="external noopener" href="https://fatcat.wiki/release/bev3bgzcvzah5dtrjiiqi6t7ty">fatcat:bev3bgzcvzah5dtrjiiqi6t7ty</a> </span>
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Finite-Time Control for Attitude Tracking Maneuver of Rigid Satellite

Mingyi Huo, Xing Huo, Hamid Reza Karimi, Jianfei Ni
<span title="">2014</span> <i title="Hindawi Limited"> <a target="_blank" rel="noopener" href="https://fatcat.wiki/container/dgcr32e3abazpn7i4ocwedp3fa" style="color: black;">Abstract and Applied Analysis</a> </i> &nbsp;
The attitude tracking performance with application of the control scheme is evaluated through a numerical example.  ...  The problem of finite-time control for attitude tracking maneuver of a rigid spacecraft is investigated. External disturbance, unknown inertia parameters are addressed.  ...  Acknowledgments This present work was supported partially by National Natural Science Foundation of China (Project no. 61304149) and Natural Science Foundation of Liaoning, China (Project no. 2013020044  ... 
<span class="external-identifiers"> <a target="_blank" rel="external noopener noreferrer" href="https://doi.org/10.1155/2014/302982">doi:10.1155/2014/302982</a> <a target="_blank" rel="external noopener" href="https://fatcat.wiki/release/q5gnjbvkrraizkvih5x6z7erbi">fatcat:q5gnjbvkrraizkvih5x6z7erbi</a> </span>
<a target="_blank" rel="noopener" href="https://web.archive.org/web/20200309111422/https://uia.brage.unit.no/uia-xmlui/bitstream/handle/11250/227247/Karimi_2014_Finite-time.pdf?sequence=1" title="fulltext PDF download" data-goatcounter-click="serp-fulltext" data-goatcounter-title="serp-fulltext"> <button class="ui simple right pointing dropdown compact black labeled icon button serp-button"> <i class="icon ia-icon"></i> Web Archive [PDF] <div class="menu fulltext-thumbnail"> <img src="https://blobs.fatcat.wiki/thumbnail/pdf/a0/86/a08651a272d79dd8dc2a851784d563496b8b5319.180px.jpg" alt="fulltext thumbnail" loading="lazy"> </div> </button> </a> <a target="_blank" rel="external noopener noreferrer" href="https://doi.org/10.1155/2014/302982"> <button class="ui left aligned compact blue labeled icon button serp-button"> <i class="unlock alternate icon" style="background-color: #fb971f;"></i> hindawi.com </button> </a>

TDE-Based Adaptive Integral Sliding Mode Control of Space Manipulator for Space-Debris Active Removal

Zhibin Zhang, Xinhong Li, Xun Wang, Xin Zhou, Jiping An, Yanyan Li
<span title="2022-02-16">2022</span> <i title="MDPI AG"> <a target="_blank" rel="noopener" href="https://fatcat.wiki/container/bnqw7sgwrve3dace7vnhziq654" style="color: black;">Aerospace (Basel)</a> </i> &nbsp;
Adaptive sliding mode control (ASMC) is used as desired injecting dynamics to compensate TDE errors, and a PID-type integral sliding mode surface is designed to reduce steady-state errors.  ...  To solve this challenge, this study examines the stabilization control of a space manipulator after capturing non-cooperative large-scale space debris and presents an adaptive integral sliding mode control  ...  Lee proposed an adaptive integral sliding mode control (AISMC) with TDE, and the dynamic injection part uses adaptive gain dynamics to achieve applicable high tracking accuracy, but the finite-time stability  ... 
<span class="external-identifiers"> <a target="_blank" rel="external noopener noreferrer" href="https://doi.org/10.3390/aerospace9020105">doi:10.3390/aerospace9020105</a> <a target="_blank" rel="external noopener" href="https://fatcat.wiki/release/mbkq63f4fvc6pjdnwyqfraf4ta">fatcat:mbkq63f4fvc6pjdnwyqfraf4ta</a> </span>
<a target="_blank" rel="noopener" href="https://web.archive.org/web/20220501143348/https://mdpi-res.com/d_attachment/aerospace/aerospace-09-00105/article_deploy/aerospace-09-00105.pdf?version=1644991933" title="fulltext PDF download" data-goatcounter-click="serp-fulltext" data-goatcounter-title="serp-fulltext"> <button class="ui simple right pointing dropdown compact black labeled icon button serp-button"> <i class="icon ia-icon"></i> Web Archive [PDF] <div class="menu fulltext-thumbnail"> <img src="https://blobs.fatcat.wiki/thumbnail/pdf/86/56/86568d12b841d1b7d769e9e42fcb65c4a99ebcd2.180px.jpg" alt="fulltext thumbnail" loading="lazy"> </div> </button> </a> <a target="_blank" rel="external noopener noreferrer" href="https://doi.org/10.3390/aerospace9020105"> <button class="ui left aligned compact blue labeled icon button serp-button"> <i class="unlock alternate icon" style="background-color: #fb971f;"></i> mdpi.com </button> </a>

Fault-Tolerant Stabilization of a Tethered Satellite System Using Offset Control

Godard, Krishna Dev Kumar, Bo Tan
<span title="">2008</span> <i title="American Institute of Aeronautics and Astronautics (AIAA)"> <a target="_blank" rel="noopener" href="https://fatcat.wiki/container/rq5e3ewv7bgrnf57ibetvdgysa" style="color: black;">Journal of Spacecraft and Rockets</a> </i> &nbsp;
The results were compared with a linear controller for which the performance deteriorated under the presence of external disturbances. 3) The adaptive sliding mode controller developed in case | damped  ...  The desired attitude of the spacecraft is ensured through regulated motion of the tether attachment points a, and a Nominal Sliding Mode Control Sliding mode control is a robust nonlinear feedback control  ... 
<span class="external-identifiers"> <a target="_blank" rel="external noopener noreferrer" href="https://doi.org/10.2514/1.35029">doi:10.2514/1.35029</a> <a target="_blank" rel="external noopener" href="https://fatcat.wiki/release/no7j7sxpyrgtfpzl5pmnruflia">fatcat:no7j7sxpyrgtfpzl5pmnruflia</a> </span>
<a target="_blank" rel="noopener" href="https://archive.org/details/sim_journal-of-spacecraft-and-rockets_september-october-2008_45_5/page/1070" title="read fulltext microfilm" data-goatcounter-click="serp-fulltext" data-goatcounter-title="serp-fulltext"> <button class="ui simple right pointing dropdown compact black labeled icon button serp-button"> <i class="icon ia-icon"></i> Archive [Microfilm] <div class="menu fulltext-thumbnail"> <img src="https://archive.org/serve/sim_journal-of-spacecraft-and-rockets_september-october-2008_45_5/__ia_thumb.jpg" alt="fulltext thumbnail" loading="lazy"> </div> </button> </a> <a target="_blank" rel="external noopener noreferrer" href="https://doi.org/10.2514/1.35029"> <button class="ui left aligned compact blue labeled icon button serp-button"> <i class="external alternate icon"></i> Publisher / doi.org </button> </a>
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