session P

Title: Poster Session
Date: 2014-10-01
Time: 13:15
Room: Prefunction

papers
Order	Paper title	Presentation status	Speaker	Affiliation	Country
1	optimal wiring configuration of multiple piezoelectric transducers for ssdi vibration suppression	confirmed	Mr. Shigeru Shimose	Japan Aerospace Exploration Agency (JAXA)	Japan
2	Researches into the Mechanical Characteristics and Optimization of the Linkage of a Strap-on Launcher	withdrawn	Dr. Shao-wei Feng	China Academy of Launch Vehicle Technology (CALT)	China
3	Optimization of the multiple payloads adapter structure configuration	confirmed	Dr. Xinyu Zhang	Beijing Institute of Aerospace Systems Engineering, China Aerospace Science and Technology Corporation (CASC)	China
4	Internal Pressure Design of Hypersonic Reusable Space Vehicle	confirmed	Dr. Pengfei Guo	China Academy of Launch Vehicle Technology(CALT)	China
5	Connection Structure Design of Hanging Cryogenic Liquid Propellants Tank of Space Vehicle	confirmed	Dr. Pengfei Guo	China Academy of Launch Vehicle Technology(CALT)	China
6	structural optimization of nano-porous insulation materials	confirmed	Prof. Zijun Hu	Aerospace Research Institute of Materials and Processing Technology(ARIMP)	China
7	solar sails: a comparative study between kapton hn and kapton b membranes	confirmed	Dr. Susanna Laurenzi	Sapienza Università di Roma	Italy
8	A New Identification Method for Multi-DOF Dynamic Interface Forces		Mr. yongtao zhang	Shanghai Institute of Satellite Engineering	China
9	plastic zone at the mixed mode crack tip in nickel-based single crystal plate based on a modified yield criterion	confirmed	Ms. lihong yang		China
10	the improved failure mode effects and criticality analysis method based on analytic hierarchy process	confirmed	Dr. lin ye		China
11	a code validation on hypersonic shock/boundary layer interaction Flows over a hollow cylinder/flare configuration		Mr. Gong Anlong		China
12	parameter optimization of the transition zone of large thin-walled tank structure	withdrawn	Mr. Ling Zhang	Beijing Institute of Aerospace Systems Engineering, China Aerospace Science and Technology Corporation (CASC)	China
13	The analysis of SH-waves propagation behaviors in periodic piezomagnetic-piezoelectric composite materials	confirmed	Mr. wei yi wei	China Academy of Launch Vehicle Technology (CALT)	China
14	An assembly tolerance analysis and optimization method based on Monte Carlo Simulation	confirmed	Mr. JIAN XU	China Academy of Launch Vehicle Technology (CALT)	China
15	The effects of stacking sequence of the skin and stiffener upon the delamination growth process for composite advanced grid stiffened structures (AGS)		Ms. Jin Yu	Beijing Institute of Structure and Environmental Engineering (BISE)	China
16	Microstructure analysis of three-dimensional full five-directional braided composites	confirmed	Dr. Fan Zhang	Research & Development Center of China Academy of Launch Vehicle Technology	China
17	application of partial least squares regression method for mathematical modeling of rocket aerodynamic data		Dr. Weiqi Qian	China Aerodynamics Research and Developement Center	China
18	optimal control for shape and vibration of space intelligent truss structure with piezoelectric actuators	confirmed	Mr. Guangbin Xun	School of Aeronautics and Astronautics, Dalian University of Technology	China
19	investigation of the aerodynamic characteristic during folded rudder deployment	confirmed	Mr. YueLong He	China Academy of Aerospace Aerodynamics (CAAA)	China
20	Thermal state of solar sail with strain-dependent optical parameters	withdrawn	Mr. Nikolay Nerovny	Bauman Moscow State Technical University	Russian Federation
21	Integrative optimized design of highly reliable repetitive folding spatial mechanism and structure	confirmed	Mr. Yue Wang	Chinese Society of Astronautics (CSA)	China
22	dynamic modeling of heat transfer in thermal-acoustic fatigue tests of hypersonic and re-entry vehicles		Prof. Xun Huang	China Academy of Aerospace Aerodynamics (CAAA)	China
23	dynamic singular modeling, robust fuzzy sliding control and flexible vibration active suppression for free-floating space robot with flexible joint and flexible manipulator	confirmed	Dr. Limin Xie	Fujian Agriculture and Forestry University	China
24	Arc-heated Experimental Method Investigation on the Scramjet Combustor Wall Thermal Protection Material	confirmed	Mr. Jian-qiang Tu	China Academy of Aerospace Aerodynamics (CAAA)	China
25	Testing of Combustor Chamber Material in Arc Jet Flow Mixing with Transverse Injected Water	confirmed	Mr. Jian-qiang Tu	China Academy of Aerospace Aerodynamics (CAAA)	China
26	Thermal Analysis of a Satellite Borne Antenna		Dr. Bo Chen	National Space Science Center, Chinese Academy of Sciences	China
27	analytic design of the phase change material for thermal control of the satellite component in periodic duty	confirmed	Prof. Taig Young Kim	Korea Polytechnic University	Korea, Republic of
28	A new concept variable resistance radiator	confirmed	Mr. Davide Paganini	University of Padova	Italy
29	Thermal Modeling of CubeSat Standard NanoSatellites	withdrawn	Mr. Anwar Ali	Politecnico di Torino	Italy
30	Equilibrium Molecular Dynamics Modeling of Diffussion and Adsorption of Fluids in Armchair Single Walled Carbon-nanotube	confirmed	Mr. Michael Kio	Cranfield University	United Kingdom
31	DEVELOPMENT OF A THERMAL CONTROL SYSTEM FOR SOUTH AFRICA'S NEXT GENERATION EARTH OBSERVATION SATELLITE	confirmed	Mr. Daniël van der Merwe	DENEL Spaceteq	South Africa
32	Arc-heating Test Simulation Method of Engine Thermal Barrier Coating (TBC) Materials with High-emissivity Rear Coating	confirmed	Mr. Jian-qiang Tu	China Academy of Aerospace Aerodynamics (CAAA)	China
33	A Case Study on the Deployment Process for Inflatable Support Booms		Mr. Manpreet Puri	University of Strathclyde	United Kingdom
34	Design and optimization of variable density multilayer insulation for cryogenic tank	confirmed	Mr. Xiaoyu Zhang	China Academy of Launch Vehicle Technology(CALT)	China
35	Simulative and experimental study of plasma distribution of Electric Propulsion Thruster		Dr. Qin Xiaogang		China
36	Design and Performance Evaluation of Reusable Launch Vehicle Aerodynamic Layout		Mr. zhang hui	China Academy of Launch Vehicle Technology (CALT)	China
37	Optimization of stiffened shell structures with stability objective/constraint based on kriging surrogate model and the explicit FEM	confirmed	Dr. bin wang	Beijing Institute of Aerospace Systems Engineering, China Aerospace Science and Technology Corporation (CASC)	China
38	studies on aero thermodynamics performance in the gap between the base side and the baseboard of air rudders in arc wind tunnel	confirmed	Mr. Kao XU	China Academy of Aerospace Aerodynamics (CAAA)	China
39	Nanocomposites for EMI shielding: A Comparative Study of EMI Shielding Properties of Carbon fillers, and Multi-Walled Carbon Nanotube Filled Polymer Composites	confirmed	Dr. Sohaib Akbar	SUPARCO	Pakistan
40	Observer-based augmented singular perturbation adaptive control of free-floating flexible space manipulator	confirmed	Dr. xiaoyan yu	Fuzhou University	China
41	flexural wave scattering by a circular hole in rectangle thin plate	withdrawn	Prof. Hongliang Li	Harbin Engineering University	China
42	Ink-jetted functional circuitry for heaters and strain-gauges aerospace applications	withdrawn	Dr. Ciro Borriello	Aviospace S.R.L	Italy
43	Optimization of High Damping Composite Fixing Panel for Launch Vehicle Electronic Apparatus	withdrawn	Prof. Yunfeng Zhao	Aerospace Research Institute of Materials & Processing Technology, China Aerospace Science and Technology Corporation (CASC)	China
44	Pulsating heat pipe for thermal control of spacecraft electronics cooling: theoretical and experimental investigations	confirmed	Mr. Zhihu Xue	China Academy of Aerospace Aerodynamics (CAAA)	China
45	analysis of large flexible spacecraft elastic vibration model and impact on attitude control system		Mr. Dayu ZHANG	Northwestern Polytechnical University	China
46	Graphene/DNA nanostructured films for bioinspired sensing of UV radiation effects	confirmed	Dr. M. Gabriella Santonicola	Sapienza Università di Roma	Italy
47	The Control-Oriented Aerodynamic Design and Analysis for Hypersonic Waverider	confirmed	Dr. Yi Li	China Academy of Launch Vehicle Technology(CALT)	China
48	curvature control of membrane laminated film structure with sputtering	withdrawn	Mr. Yuki Teramoto	Department of Engineering, The University of Tokyo	Japan
49	investigation of fairing typical attitude aerodynamic characteristic during fairing separation	confirmed	Dr. Dun Li	China Academy of Aerospace Aerodynamics (CAAA)	China
50	Modeling and Analysis of Reinforced Membranes for Space Applications	confirmed	Dr. Hang Shi	Aerospace System Engineering Shanghai	China
51	Structural performance and helium / hydrogen permeability rates of fused deposition modeling polymers at cryogenic temperatures	withdrawn	Mr. Patrick Adam	Washington State University	United States
52	ablative performance comparison study of lightweight and dense 3d carbon fabric composites		Dr. Yunhua Yang	Aerospace Research Institute of Materials and Processing Technology(ARIMP)	China
53	the research of solar wing deployment support mechanism based on the tape spring		Dr. xiaoguang xie	CAS	China
54	Evaluation and Test of Polyamide Gears for Pointing Mechanisms	withdrawn	Mr. Ralf Purschke	Technische Universität München	Germany
55	analysis of boundary layer suppression in unsymmetrical airfoil using piezo electric effect		Mr. MADHAN RAJ	Hindustan University	India
56	identification of damaged configurations in a truss-type structure	confirmed	Dr. Davide Nardi	University of Rome "La Sapienza"	Italy
57	Accurate satellite mathematical model generation for line of sight jitter evaluation using semi-direct updating techniques with modal survey test	confirmed	Dr. Jae Hyuk Lim	Korea Aerospace Research Institute (KARI)	Korea, Republic of
58	triangle-section coilable mast development for buaa-sat	confirmed	Mr. Ma Haibo	Beihang University	China
59	A few varieties of measurement methods for testing composite structures	confirmed	Ms. lina mao	Beijing Institute of Structure and Environment Engineering	China
60	the POGO stability analysis of large liquid rocket considering longitudinal, lateral and torsional mode in structural system	confirmed	Dr. Qingwei Wang	Dalian University of Technology (DUT)	China
61	spectral dependency of polarization properties for the lunar regolith	confirmed	Mr. Minsup Jung	Kyung Hee University	Korea, Republic of
62	Thermal Designing and Analysis Using ANSYS for ‘Pratham’ Student Satellite IIT Bombay	confirmed	Mr. Ratnesh Mishra	Indian Institute of Technology	India
63	Model-free control for active multi-mode vibration confinement of spaceborne truss using a six-degree-of-freedom Stewart platform		Mr. Gaonan Xu	Beihang University	China
64	New reinforcement method of impact bruising alloy thin-wall tank	withdrawn	Mrs. xiaoying zhang	Beijing Institute of Astronautical Systems Enginnering	China
65	Preliminary Thermal and Orbital Spin Analysis of NanoSatellites	withdrawn	Mr. Anwar Ali	Politecnico di Torino	Italy
66	Study on Prediction Method of Aerodynamic Characteristics Analysis for Mars Entry Capsules	confirmed	Mrs. Huiling Zhan	China Academy of Aerospace Aerodynamics (CAAA)	China
67	Integrated design proposal for a lightweight and efficient heat protection and insulation technology	confirmed	Dr. Fei Wang	China Academy of Launch Vehicle Technology (CALT)	China
68	dynamics modeling and radial basis function neural network adaptive control of dual-arm flexible-joint space robot with parameter unknown		Ms. Pin Liang		China
69	INCREASED ZERO REACTION WORKSPACE OF A HYPER-REDUNDANT FREE-FLOATING SPACE ROBOT	withdrawn	Dr. Silvio Cocuzza	CISAS – “G. Colombo” Center of Studies and Activities for Space, University of Padova	Italy
70	Biochemical detector based on the controlled tunneling between detector nanostructures and analyte		Prof. Branislav Vlahovic	North Carolina Central University	United States
71	heat transfer characteristic of confined jet array impingement cooling for high heat flux applications of spacecraft		Dr. Gang Chen	Shanghai Insitute of Satellite Engineering	China
72	Study on large launch vehicle segmengts connected by bolts		Mr. Zhou hongxi		China
73	An Improved Test System for Thermal-Structural Test of Thin Shell Parts of Spacecraft.
74	CEVHER - Vertical Take-Off Landing (VTOL) with Coanda Effect		Mr. Cagri Kilic	Gumush Aerospace & Defense	Türkiye
75	Capillary infiltration behavior of C/C-preforms for production of C/C-SiC composites via LSI		Dr. Xiaojun WU		China
76	High-precision temperature control method study based on hiberarchy thermal control		Mr. song jialiang	Department of Thermal Science and Energy Engineering, University of Science and Technology of China	China
77	research on passive orbital disconnect structs of cryogenic tank	withdrawn	Ms. DONG Xiaolin	China Academy of Launch Vehicle Technology(CALT)	China
78	analysis and verification of satellite thermal deformation influence on positioning accuracy		Dr. ming li		China
79	investigation of ablative properties of lightweight carbon/phenolic composites		Dr. Yun Wang	Aerospace Research Institute of Materials and Processing Technology(ARIMP)	China
80	The synthesis and pyrolysis mechanism of resole phenolic resin for ablative materials		Mr. Dawei Han	Aerospace Research Institute of Materials and Processing Technology(ARIMP)	China
81	Deployment Dynamics of a Large Deployable Mesh Antenna Considering Anti-entanglement Techniques	confirmed	Mr. Zhicheng Zhou	China Academy of Space Technology (CAST)	China
–	research on unit sine vibration test level of spacecraft		Dr. Hong Lin	Beijing Institute of Aerospace Systems Engineering, China Aerospace Science and Technology Corporation (CASC)	China

session P

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