Robust adaptive relative position tracking and attitude synchronization for spacecraft rendezvous (English)
- New search for: Sun, Liang
- New search for: Huo, Wei
- New search for: Sun, Liang
- New search for: Huo, Wei
In:
Aerospace Science and Technology
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41
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28-35
;
2014
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ISSN:
- Article (Journal) / Electronic Resource
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Title:Robust adaptive relative position tracking and attitude synchronization for spacecraft rendezvous
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Contributors:Sun, Liang ( author ) / Huo, Wei ( author )
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Published in:Aerospace Science and Technology ; 41 ; 28-35
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Publisher:
- New search for: Elsevier Masson SAS
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Publication date:2014-11-22
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Size:8 pages
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ISSN:
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DOI:
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Type of media:Article (Journal)
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Type of material:Electronic Resource
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Language:English
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Keywords:
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Source:
Table of contents – Volume 41
The tables of contents are generated automatically and are based on the data records of the individual contributions available in the index of the TIB portal. The display of the Tables of Contents may therefore be incomplete.
- 1
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Investigation of structural stability characteristics of high speed underwater vehicles according to mass changeKong, Changduk / Oh, Kyungwon / Park, Hyunbum et al. | 2014
- 7
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Thermal buckling analysis of functionally graded rectangular nanoplates based on nonlocal third-order shear deformation theoryNami, Mohammad Rahim / Janghorban, Maziar / Damadam, Mohsen et al. | 2014
- 16
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Diving guidance via feedback linearization and sliding mode controlLiu, Luhua / Zhu, Jianwen / Tang, Guojian / Bao, Weimin et al. | 2014
- 24
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Preheating characteristics of H2O2 monopropellant thruster using manganese oxide catalystJang, Dongwook / Kang, Shinjae / Kwon, Sejin et al. | 2014
- 28
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Robust adaptive relative position tracking and attitude synchronization for spacecraft rendezvousSun, Liang / Huo, Wei et al. | 2014
- 36
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Coupling dynamics modelling and optimal coordinated control of tethered space robotHuang, Panfeng / Hu, Zehong / Meng, Zhongjie et al. | 2014
- 47
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Nonlinear analysis of functionally graded nanocomposite rotating thick disks with variable thickness reinforced with carbon nanotubesZafarmand, Hassan / Kadkhodayan, Mehran et al. | 2014
- 55
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Control of combustion instability with a tunable Helmholtz resonatorZhang, Zhiguo / Zhao, Dan / Han, Nuomin / Wang, Shuhui / Li, Junwei et al. | 2014
- 63
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Data and design models for military turbo-propeller aircraftMarinus, Benoît G. / Poppe, Joachim et al. | 2014
- 81
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Design of an adaptive Kalman filter to eliminate measurement faults of a laser rangefinder used in the UAV systemKownacki, Cezary et al. | 2014
- 90
-
Nonlinear bending analysis of FGM circular plates based on physical neutral surface and higher-order shear deformation theoryZhang, Da-Guang / Zhou, Hao-Miao et al. | 2014
- 99
-
Investigation of interior ballistics and performance analysis of hydro-reactive motorsGhassemi, Hojat / Farshi Fasih, Hamidreza et al. | 2014
- 106
-
Neural network modeling of unsteady aerodynamic characteristics at high angles of attackIgnatyev, Dmitry I. / Khrabrov, Alexander N. et al. | 2014
- 116
-
Real-time validation of Indian Remote Sensing Satellite data down link chain performance and evaluation of online data analysis with BER measurementSrinivas, R. / Nithyananadan, L. / Subba Rao, P.V.V. / Umadevi, G. et al. | 2014
- 122
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Active gust load alleviation system for flexible aircraft: Mixed feedforward/feedback approachAlam, Mushfiqul / Hromcik, Martin / Hanis, Tomas et al. | 2014
- 134
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Numerical studies on plasma plume flows from a cluster of electric propulsion devicesCai, Chunpei et al. | 2014
- 144
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X-ray pulsar/Doppler difference integrated navigation for deep space exploration with unstable solar spectrumLiu, Jin / Fang, Jian-cheng / Yang, Zhao-hua / Kang, Zhi-wei / Wu, Jin et al. | 2014
- 151
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Stall inception and control in a transonic fan, part B: Stall control by discrete endwall injectionKhaleghi, Hossein et al. | 2014
- 158
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Electrode grouping optimization of electrostatic forming membrane reflector antennasZhang, Yiqun / Gao, Feng / Zhang, Shuxin / Hao, Jia et al. | 2014
- 167
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Robust air velocity estimation based on iterative implementation of Minimum Mean-Square Error (MMSE)Yu, F. / Tao, J.W. / Yang, Y.M. et al. | 2014
- 175
-
High maneuverability projectile flight using low cost componentsFresconi, Frank / Celmins, Ilmars / Silton, Sidra / Costello, Mark et al. | 2014
- 189
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Towards modelling ultraviolet index in global scale. Artificial neural networks approachLatosińska, Jolanta Natalia / Latosińska, Magdalena / Bielak, Jarosław et al. | 2014
- 199
-
Continuous second-order sliding mode based impact angle guidance lawHe, Shaoming / Lin, Defu / Wang, Jiang et al. | 2014
- 209
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Nonlinear feedback control of self-sustained thermoacoustic oscillationsRubio-Hervas, Jaime / Zhao, Dan / Reyhanoglu, Mahmut et al. | 2014
- 216
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Adjoint shape optimization of airfoils with attached Gurney flapAmini, Y. / Emdad, H. / Farid, M. et al. | 2014
- 229
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An adjoint-truncation error based approach for goal-oriented mesh adaptationPonsin, J. / Fraysse, F. / Gómez, M. / Cordero-Gracia, M. et al. | 2014
- 241
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Adjoint quasi-three-dimensional aerodynamic solver for multi-fidelity wing aerodynamic shape optimizationElham, Ali et al. | 2014
- 250
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Stall inception and control in a transonic fan, part A: Rotating stall inceptionKhaleghi, Hossein et al. | 2014
- 259
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Numerical design and analysis of a multi-DBD actuator configuration for the experimental testing of ACHEON nozzle modelAbdollahzadeh, M. / Rodrigues, F. / Pascoa, J.C. / Oliveira, P.J. et al. | 2014
- 274
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Rarefied gas flow simulations of NACA 0012 airfoil and sharp 25–55-deg biconic subject to high order nonequilibrium boundary conditions in CFDLe, Nam T.P. / Shoja-Sani, Ahmad / Roohi, Ehsan et al. | 2014
- 289
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Guidance and control for satellite in-orbit-self-assembly proximity operationsOkasha, Mohamed / Park, Chandeok / Park, Sang-Young et al. | 2014
- IFC
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Editorial Board| 2015