A high accuracy multiplex two-position alignment method based on SINS with the aid of star sensor (English)
- New search for: Wang, Xinlong
- New search for: Wang, Xinlong
- New search for: Guan, Xujun
- New search for: Fang, Jiancheng
- New search for: Li, Hengnian
In:
Aerospace science and technology
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42
; 66-73
;
2015
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ISSN:
- Article (Journal) / Print
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Title:A high accuracy multiplex two-position alignment method based on SINS with the aid of star sensor
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Contributors:
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Published in:Aerospace science and technology ; 42 ; 66-73
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Publisher:
- New search for: Elsevier
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Place of publication:Paris
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Publication date:2015
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ISSN:
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ZDBID:
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DOI:
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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: 55.50 / 55.60
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Source:
Table of contents – Volume 42
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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Integrated guidance and control law for cooperative attack of multiple missilesWang, Xiaofang / Zheng, Yiyu / Lin, Hai et al. | 2014
- 12
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Linear and nonlinear control strategies for formation and station keeping of spacecrafts within the context of the three body problemDarvish, Kourosh / Pourtakdoust, Seid H. / Assadian, Nima et al. | 2014
- 25
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Specific force integration algorithm with high accuracy for strapdown inertial navigation systemLin, Yurong / Zhang, Wei / Xiong, Jianqiong et al. | 2015
- 31
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Hierarchical modeling and optimization of camber morphing airfoilMurugan, Senthil / Woods, B.K.S. / Friswell, M.I. et al. | 2014
- 39
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Concurrent subspace design optimization and analysis of hypersonic vehicles based on response surface modelsZhang, Dong / Tang, Shuo / Che, Jing et al. | 2015
- 50
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Rigid spacecraft attitude control using adaptive integral second order sliding modeTiwari, Pyare Mohan / Janardhanan, S. / un Nabi, Mashuq et al. | 2014
- 58
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Evaluating military training aircrafts through the combination of multi-criteria decision making processes with fuzzy logic. A case study in the Spanish Air Force AcademySánchez-Lozano, J.M. / Serna, J. / Dolón-Payán, A. et al. | 2014
- 66
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A high accuracy multiplex two-position alignment method based on SINS with the aid of star sensorWang, Xinlong / Guan, Xujun / Fang, Jiancheng / Li, Hengnian et al. | 2014
- 74
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Modal behavior of a new large reflector conceptual designMorterolle, Sébastien / Maurin, Bernard / Dube, Jean-François / Averseng, Julien / Quirant, Jérôme et al. | 2015
- 80
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Liquefying fuel regression rate modeling in hybrid propulsionLestrade, J.-Y. / Anthoine, J. / Lavergne, G. et al. | 2014
- 88
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Positioning performance analysis using RWLS algorithm based on variance estimation methodsMosavi, M.R. / Rahemi, N. et al. | 2014
- 97
-
Relative attitude and position estimation for a tumbling spacecraftZhang, Lijun / Zhang, Shifeng / Yang, Huabo / Cai, Hong / Qian, Shan et al. | 2014
- 106
-
Aerodynamic design optimization of helicopter rotor blades including airfoil shape for forward flightVu, N.A. / Lee, J.W. et al. | 2014
- 118
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Aeroelastic analysis and active flutter suppression of an electro-rheological sandwich cylindrical panel under yawed supersonic flowHasheminejad, Seyyed M. / Aghayi Motaaleghi, M. et al. | 2015
- 128
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Variable geometry cowl sidewall for improving rectangular hypersonic inlet performanceTeng, Jian / Yuan, Huacheng et al. | 2015
- 136
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Multi-fidelity optimization strategy for the industrial aerodynamic design of helicopter rotor bladesLeusink, Debbie / Alfano, David / Cinnella, Paola et al. | 2015
- 148
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Low frequency instability in laboratory-scale hybrid rocket motorsPark, Kyung-Su / Lee, Changjin et al. | 2015
- 158
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Numerical study of shock/boundary layer interaction in supersonic overexpanded nozzlesHadjadj, A. / Perrot, Y. / Verma, S. et al. | 2015
- 169
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Experimental study on the effect of combustor configuration on the performance of dual-mode combustorWang, Z.P. / Li, F. / Gu, H.B. / Yu, X.L. / Zhang, X.Y. et al. | 2015
- 176
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Simple finite-time attitude stabilization laws for rigid spacecraft with bounded inputsGui, Haichao / Jin, Lei / Xu, Shijie et al. | 2015
- 187
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Simplified brain storm optimization approach to control parameter optimization in F/A-18 automatic carrier landing systemLi, Junnan / Duan, Haibin et al. | 2015
- 196
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Optimization and analysis of shock wave/boundary layer interaction for drag reduction by Shock Control BumpMazaheri, K. / Kiani, K.C. / Nejati, A. / Zeinalpour, M. / Taheri, R. et al. | 2015
- 209
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The Adaptive Aspect Ratio morphing wing: Design concept and low fidelity skin optimizationWoods, Benjamin K.S. / Friswell, Michael I. et al. | 2015
- 218
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Numerical simulations and performance assessment of a scramjet powered cruise vehicle at Mach 8Roncioni, Pietro / Natale, Pasquale / Marini, Marco / Langener, Tobias / Steelant, Johan et al. | 2015
- 229
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Finite element analysis for acoustic characteristics of combustion stabilization devicesKim, Seong-Ku / Choi, Hwan Seok / Kim, Hong Jip / Ko, Young Sung / Sohn, Chae Hoon et al. | 2015
- 241
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Output feedback control of Lorentz-augmented spacecraft rendezvousHuang, Xu / Yan, Ye / Zhou, Yang / Yu, Jinlong et al. | 2015
- 249
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Robust multiple model adaptive estimation for spacecraft autonomous navigationXiong, K. / Wei, C.L. / Liu, L.D. et al. | 2015
- 259
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Switching robust control for a nanosatellite launch vehicleLu, Bei / Falde, Derek / Iriarte, Estuardo / Besnard, Eric et al. | 2015
- 267
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Effect of aspect ratio on wing rock at low Reynolds numberGo, Tiauw Hiong / Maqsood, Adnan et al. | 2015
- 274
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Real-time estimation of helicopter blade kinematics using integrated linear displacement sensorsAllred, C. Jefferson / Jolly, Mark R. / Buckner, Gregory D. et al. | 2014
- 287
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Regression rate and combustion performance investigation of aluminum metallized HTPB/98HP hybrid rocket motor with numerical simulationSun, Xingliang / Tian, Hui / Yu, Nanjia / Cai, Guobiao et al. | 2015
- 297
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Novel approach for design of a waverider vehicle generated from axisymmetric supersonic flows past a pointed von Karman ogiveDing, Feng / Liu, Jun / Shen, Chi-bing / Huang, Wei et al. | 2015
- 309
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Adaptive velocity synchronization compound control of electro-hydraulic load simulatorWang, Chengwen / Jiao, Zongxia / Quan, Long et al. | 2015
- 322
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Condition-based flight control for helicopters: An extension to condition-based maintenanceVoskuijl, Mark / van Tooren, Michel J.L. / Walker, Daniel J. et al. | 2015
- 334
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Ignition theory investigation and experimental research on hybrid rocket motorTian, Hui / Li, Xintian / Cai, Guobiao et al. | 2015
- 342
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Deployment and control of spacecraft solar array considering joint stick-slip frictionLi, Hai-Quan / Liu, Xiao-Feng / Duan, Liu-Cheng / Cai, Guo-Ping et al. | 2015
- 353
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Tracking control of spacecraft formation flying with collision avoidanceHu, Qinglei / Dong, Hongyang / Zhang, Youmin / Ma, Guangfu et al. | 2014
- 365
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Design and optimization of low-thrust orbital phasing maneuverShang, Haibin / Wang, Shuai / Wu, Weiren et al. | 2015
- 376
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Generation of Richtmyer–Meshkov and secondary instabilities during the interaction of an energy release with a cylinder shock layerAzarova, O.A. et al. | 2015
- 384
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Nonlinear dynamics of a rotating triangular tethered satellite formation near libration pointsCai, Zhiqin / Li, Xuefu / Zhou, Hong et al. | 2015
- 392
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Measured aerodynamic characteristics of wings at low Reynolds numbersAnanda, G.K. / Sukumar, P.P. / Selig, M.S. et al. | 2014
- 407
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Drag and heat reduction mechanism in the combinational opposing jet and acoustic cavity concept for hypersonic vehiclesHuang, Wei / Yan, Li / Liu, Jun / Jin, Liang / Tan, Jian-guo et al. | 2015
- 415
-
Artificial neural network based inverse design: Airfoils and wingsSun, Gang / Sun, Yanjie / Wang, Shuyue et al. | 2015
- 429
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Active robust control of uncertainty and flexibility suppression for air-breathing hypersonic vehiclesPu, Zhiqiang / Yuan, Ruyi / Tan, Xiangmin / Yi, Jianqiang et al. | 2015
- 442
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Robust gain scheduled control of spacecraft rendezvous system subject to input saturationWang, Qian / Zhou, Bin / Duan, Guang-Ren et al. | 2015
- 451
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Dynamic stability conditions for a rolling flight vehicle applying continuous actuatorKoohmaskan, Yousof / Arvan, Mohammad Reza / Vali, Ahmad Reza / Behazin, Farid et al. | 2015
- 459
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A parametric study of fixed-wing aircraft perching maneuversVenkateswara Rao, D.M.K.K. / Tang, Hui / Go, Tiauw Hiong et al. | 2015
- 470
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Vibration tests on the preloaded LARES satellite and separation systemParis, Claudio et al. | 2015
- 477
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Robust gain-scheduled autopilot design for spin-stabilized projectiles with a course-correction fuzeTheodoulis, Spilios / Sève, Florian / Wernert, Philippe et al. | 2014
- IFC
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Editorial Board| 2015