A rapid and high precise calibration method for long-distance cruise missiles (English)
- New search for: Wang, X.
- New search for: Wang, B.
- New search for: Wu, X.
- New search for: Wang, X.
- New search for: Wang, B.
- New search for: Wu, X.
In:
AEROSPACE SCIENCE AND TECHNOLOGY
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27
, 1
;
1-9
;
2013
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ISSN:
- Article (Journal) / Print
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Title:A rapid and high precise calibration method for long-distance cruise missiles
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Contributors:
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Published in:AEROSPACE SCIENCE AND TECHNOLOGY ; 27, 1 ; 1-9
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Publisher:
- New search for: Elsevier Science B.V., Amsterdam.
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Publication date:2013-01-01
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Size:9 pages
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ISSN:
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Type of media:Article (Journal)
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Type of material:Print
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Language:English
- New search for: 629.105
- Further information on Dewey Decimal Classification
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Classification:
DDC: 629.105 -
Source:
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Table of contents – Volume 27, Issue 1
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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A rapid and high precise calibration method for long-distance cruise missilesWang, Xinlong / Wang, Bin / Wu, Xiaojuan et al. | 2012
- 10
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Numerical study of the spacecraft thermal control hardware combining solid–liquid phase change material and a heat pipeKim, Taig Young / Hyun, Bum-Seok / Lee, Jang-Joon / Rhee, Juhun et al. | 2012
- 17
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A stabilized optimal nonlinear feedback control for satellite attitude trackingZhang, Binbin / Liu, Kun / Xiang, Junhua et al. | 2012
- 25
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A numerical approach for the study of the gas–surface interaction in carbon–phenolic solid rocket nozzlesTurchi, A. / Bianchi, D. / Nasuti, F. / Onofri, M. et al. | 2012
- 32
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Multiple target tracking based on homogeneous symmetric transformation of measurementsSwati / Bhaumik, Shovan et al. | 2012
- 44
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Preliminary study on the aerodynamic characteristics of an adaptive reconfigurable airfoilHuang, Diangui / Wu, Guoqing et al. | 2012
- 49
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Thermal failure of the LM117 regulator under harsh space thermal environmentsSeo, H.-S. / Rhee, J. / Han, E.-S. / Kim, I.-S. et al. | 2012
- 57
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On the penetrative Benard–Marangoni convection in a ferromagnetic fluid layerNanjundappa, C.E. / Shivakumara, I.S. / Srikumar, K. et al. | 2012
- 67
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On the modeling of aircraft tireKongo Kondé, A. / Rosu, I. / Lebon, F. / Brardo, O. / Devésa, B. et al. | 2012
- 76
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Superelements for a computationally efficient structural analysis of elliptical fuselage sectionsQuatmann, M. / Aswini, N. / Reimerdes, H.-G. / Gupta, N.K. et al. | 2012
- 84
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Thermal analysis of composite solar array subjected to space heat fluxLi, Junlan / Yan, Shaoze / Cai, Renyu et al. | 2012
- 95
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Bias fusion estimation for multi-target tracking systems with multiple asynchronous sensorsHu, Y.Y. / Zhou, D.H. et al. | 2012
- 105
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Cooperative localization between small UAVs using a combination of heterogeneous sensorsLee, Wonsuk / Bang, Hyochoong / Leeghim, Henzeh et al. | 2012
- 112
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Integrated translational and rotational control for the terminal landing phase of a lunar moduleZhang, Feng / Duan, Guang-Ren et al. | 2012
- 127
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Quasi-continuous high-order sliding mode controller and observer design for flexible hypersonic vehicleZong, Qun / Wang, Jie / Tian, Bailing / Tao, Yang et al. | 2012
- 138
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Optimization of a flight-worthy scramjet combustor through CFDManna, P. / Dharavath, Malsur / Sinha, P.K. / Chakraborty, Debasis et al. | 2012
- 147
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A difference-fractional FOM decision method for down-selection of hypersonic compression system configurationsSarosh, Ali / Shi-Ming, Chen / Yun-Feng, Dong et al. | 2012
- 156
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Development of an efficient hybrid model for range sidelobe suppression in pulse compression radarBaghel, V. / Panda, G. et al. | 2012
- 163
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Thermal cycle analysis of turboelectric distributed propulsion system with boundary layer ingestionLiu, Chengyuan / Doulgeris, Georgios / Laskaridis, Panagiotis / Singh, Riti et al. | 2012
- 171
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Study on spray patterns of gas-centered swirl coaxial (GCSC) injectors in high pressure conditionsKim, Jong Gyu / Han, Yeoung Min / Choi, Hwan Seok / Yoon, Youngbin et al. | 2012
- 179
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Nanosatellite swarm missions in low Earth orbit using laser propulsionFelicetti, L. / Santoni, F. et al. | 2012
- 188
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Fatigue assessment of AA 8090 friction stir butt welds after surface finishing treatmentPedemonte, M. / Gambaro, C. / Lertora, E. / Mandolfino, C. et al. | 2012
- 193
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Galileo-based space–airborne bistatic SAR for UAS navigationRenga, Alfredo / Graziano, Maria Daniela / DʼErrico, Marco / Moccia, Antonio / Menichino, Flavio / Vetrella, Sergio / Accardo, Domenico / Corraro, Federico / Cuciniello, Giovanni / Nebula, Francesco et al. | 2012
- 201
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Airbreathing rotating detonation wave engine cycle analysisBraun, Eric M. / Lu, Frank K. / Wilson, Donald R. / Camberos, José A. et al. | 2012
- 209
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Influences of particle size and content of HMX on burning characteristics of HMX-based propellantNaya, Tomoki / Kohga, Makoto et al. | 2012
- 216
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Application of the reassignment time–frequency method on an acoustic signals backscattered by an air-filled circular cylindrical shell immersed in waterLaaboubi, M. / Aassif, E. / Latif, R. / Dliou, A. / Maze, G. / Décultot, D. et al. | 2012
- IFC
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Editorial Board| 2013