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Adaptive tracking control of spacecraft relative motion with mass and thruster uncertaintiesHYUNGJOO YOON; YOUNGHO EUN; CHANDEOK PARK et al.Aerospace science and technology (Imprimé). 2014, Vol 34, pp 75-83, issn 1270-9638, 9 p.Article
Guidance law for low-lift skip reentry subject to control saturation based on nonlinear predictive controlMINWEN GUO; DAYI WANG.Aerospace science and technology (Imprimé). 2014, Vol 37, pp 48-54, issn 1270-9638, 7 p.Article
Hybrid Control of Liquid-Filled Spacecraft Maneuvers by Dynamic Inversion and Input ShapingYUE BAOZENG; ZHU LEMEI.AIAA journal. 2014, Vol 52, Num 3, pp 618-626, issn 0001-1452, 9 p.Article
Inverse analysis for transient thermal load identification and application to aerodynamic heating on atmospheric reentry capsuleNAKAMURA, Toshiya; KAMIMURA, Yukihiro; IGAWA, Hirotaka et al.Aerospace science and technology (Imprimé). 2014, Vol 38, pp 48-55, issn 1270-9638, 8 p.Article
Low-thrust trajectory design with constrained particle swarm optimizationJINJUN SHAN; YUAN REN.Aerospace science and technology (Imprimé). 2014, Vol 36, pp 114-124, issn 1270-9638, 11 p.Article
Space station overall mission planning using decomposition approachLIN, Kun-Peng; LUO, Ya-Zhong; JIN ZHANG et al.Aerospace science and technology (Imprimé). 2014, Vol 33, pp 26-39, issn 1270-9638, 14 p.Article
Aerothermal response of ceramic matrix composites to nitrogen plasma at temperatures above 2000 KPANERAI, Francesco; HELBER, Bernd; CHAZOT, Olivier et al.Aerospace science and technology (Imprimé). 2014, Vol 39, pp 1-5, issn 1270-9638, 5 p.Article
Flow Structures and Heating Augmentation Around Finite-Width Cavity in Hypersonic FlowOHMICHI, Yuya; SUZUKI, Kojiro.AIAA journal. 2014, Vol 52, Num 8, pp 1624-1631, issn 0001-1452, 8 p.Conference Paper
Hypersonic high altitude aerothermodynamics of a space re-entry vehicleVOTTA, Raffaele; SCHETTINO, Antonio; BONFIGLIOLI, Aldo et al.Aerospace science and technology (Imprimé). 2013, Vol 25, Num 1, pp 253-265, issn 1270-9638, 13 p.Article
Experimental and numerical study on the aero-heating characteristics of blunted waveriderLIU, Jian-Xia; HOU, Zhong-Xi; CHEN, Xiao-Qing et al.Applied thermal engineering. 2013, Vol 51, Num 1-2, pp 301-314, issn 1359-4311, 14 p.Article
Impact of a submarine on the seabedPELAEZ, J. G; VALIENTE, G. R; REIJMERS, J. J et al.Transactions on the built environment. 2013, Vol v. 126, pp 357-368, issn 1746-4498, isbn 978-1-8456-4612-7, 1Vol, 12 p.Conference Paper
Formulation of Design Charts for Composite Submarine Pressure HullsSMITH, T; ROSS, T. F; LITTLE, Andrew P. F et al.Journal of ship production and design (Print). 2012, Vol 28, Num 1, pp 20-41, issn 2158-2866, 22 p.Article
Method to Control Unsteady Force of Submarine Propeller Based on the Control of Horseshoe VortexLIU ZHIHUA; XIONG YING; TU CHENGXU et al.Journal of ship research. 2012, Vol 56, Num 1, pp 12-22, issn 0022-4502, 11 p.Article
Role of Thermal Contact Conductance on Sandwich-Type Metallic Thermal Protection System ProfileRAMESH KUMAR, R; PALANINATHAN, R; KISHOR, E et al.AIAA journal. 2012, Vol 50, Num 10, pp 2194-2201, issn 0001-1452, 8 p.Article
Design and parameter estimation of a remotely operated underwater vehicleWANG, Yung-Lien; LU, Chang-Yu.Journal of marine engineering and technology. 2012, Vol 11, Num 2, pp 39-48, issn 2046-4177, 10 p.Article
Output feedback back-stepping control for a generic Hypersonic Vehicle via small-gain theoremQUN ZONG; YUEHUI JI; FANLIN ZENG et al.Aerospace science and technology (Imprimé). 2012, Vol 23, Num 1, pp 409-417, issn 1270-9638, 9 p.Article
Simultaneous optimization of staging and trajectory of launch vehicles using two different approachesJAMILNIA, Reza; NAGHASH, Abolghasem.Aerospace science and technology (Imprimé). 2012, Vol 23, Num 1, pp 85-92, issn 1270-9638, 8 p.Article
A simplified approach to design fuzzy logic controller for an underwater vehicleISHAQUE, K; ABDULLAH, S. S; AYOB, S. M et al.Ocean engineering. 2011, Vol 38, Num 1, pp 271-284, issn 0029-8018, 14 p.Article
Coupled simulation of heat transfer and temperature of the composite rocket nozzle wallZHANG XIAOYING.Aerospace science and technology (Imprimé). 2011, Vol 15, Num 5, pp 402-408, issn 1270-9638, 7 p.Article
Robust control for an autonomous underwater vehicle that suppresses pitch and yaw couplingPETRICH, Jan; STILWELL, Daniel J.Ocean engineering. 2011, Vol 38, Num 1, pp 197-204, issn 0029-8018, 8 p.Article
Reduction of Hull-Radiated Noise Using Vibroacoustic Optimization of the Propulsion SystemCARESTA, Mauro; KESSISSOGLOU, Nicole J.Journal of ship research. 2011, Vol 55, Num 3, pp 149-162, issn 0022-4502, 14 p.Article
Ngong Ping 360: Hong Kong's state-of-the-art cable carTANK, Suresh; BATCHELOR, John; SMITH, Calum et al.Proceedings of the Institution of Civil Engineers. Civil engineering. 2010, Vol 163, Num 1, pp 18-26, issn 0965-089X, 9 p.Article
Hybrid continuum/DSMC computation of rocket mode lightcraft flow in near space with high temperature and rarefaction effectXU, Shan-Shu; WU, Zi-Niu; QIAN LI et al.Computers & fluids. 2009, Vol 38, Num 7, pp 1394-1404, issn 0045-7930, 11 p.Article
Transformed equations of motion for underwater vehiclesHERMAN, Przemyslaw.Ocean engineering. 2009, Vol 36, Num 3-4, pp 306-312, issn 0029-8018, 7 p.Article
Decoupled PD set-point controller for underwater vehiclesHERMAN, Przemyslaw.Ocean engineering. 2009, Vol 36, Num 6-7, pp 529-534, issn 0029-8018, 6 p.Article