<datastore> <nextgroup><![CDATA[<a href="/module/jslib/jquery/jpage/dataproxy.jsp?page=1&appid=1&appid=1&webid=2&path='/'&columnid=1344&unitid=3691&webname='China Manned Space Engineering'&permissiontype=0"></a>]]></nextgroup> <recordset> <record><![CDATA[ <table width="705" height="110" border="0" cellspacing="0" cellpadding="8" style=" margin-bottom:10px;"> <tr> <td align="left" valign="top"><table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td height="40"> <a href='/art/2015/10/8/art_1344_22135.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">A Sinusoidal Linear Acceleration System for Calibration of Linertial Measurement Unit (IMU) Dynamic ...</a></td> </tr> </table> <table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td valign="top"><span style="line-height:22px; font-size: 15px; color:#313131">Abstract： Aiming at the difficulty of accurate calibration for inertial measure unit (IMU) dynamic error on the ground, a new calibration method for IMU dynamic error based on sinusoidal linear acceleration experimentation system was proposed. An experimentation system which could supply sinusoidal linear acceleration environment to meet the IMU test requirements was set up.</span></td> </tr> </table></td> </tr></table><table width="100%" border="0" cellspacing="0" cellpadding="0" style=" margin-bottom:10px" height="0"> <tr> <td style="border-bottom: dotted 1px #cbcbcb;" ></td> </tr></table>]]></record> <record><![CDATA[ <table width="705" height="110" border="0" cellspacing="0" cellpadding="8" style=" margin-bottom:10px;"> <tr> <td align="left" valign="top"><table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td height="40"> <a href='/art/2015/10/8/art_1344_22136.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Oxygen Production in Microalgal Reactor for Water, Air and Waste Reclamation</a></td> </tr> </table> <table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td valign="top"><span style="line-height:22px; font-size: 15px; color:#313131">Abstract ： In order to evaluate the feasibility of introducing microalgae into closed ecological system and achieving potential food production as well as air revilization and water reclaimation，NH4+-N in wastes urine was nitrified to NO3--N as proper N source for culture of edible protein，Spirulina platensis，which was utilized to absorb CO2 and produce O2.</span></td> </tr> </table></td> </tr></table><table width="100%" border="0" cellspacing="0" cellpadding="0" style=" margin-bottom:10px" height="0"> <tr> <td style="border-bottom: dotted 1px #cbcbcb;" ></td> </tr></table>]]></record> <record><![CDATA[ <table width="705" height="110" border="0" cellspacing="0" cellpadding="8" style=" margin-bottom:10px;"> <tr> <td align="left" valign="top"><table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td height="40"> <a href='/art/2015/10/8/art_1344_22137.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Space Circle of Non-cooperative Target Detection Algorithm during On-orbit Service</a></td> </tr> </table> <table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td valign="top"><span style="line-height:22px; font-size: 15px; color:#313131">Abstract: In order to complete the on-orbit service independently， various functions need to be satisfied and many key technologies be solved. This paper mainly studied the detection algorithm for the space circle of non-cooperative target such as the docking ring of satellite and rocket and engine nozzle.</span></td> </tr> </table></td> </tr></table><table width="100%" border="0" cellspacing="0" cellpadding="0" style=" margin-bottom:10px" height="0"> <tr> <td style="border-bottom: dotted 1px #cbcbcb;" ></td> </tr></table>]]></record> <record><![CDATA[ <table width="705" height="110" border="0" cellspacing="0" cellpadding="8" style=" margin-bottom:10px;"> <tr> <td align="left" valign="top"><table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td height="40"> <a href='/art/2015/10/8/art_1344_22138.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Applications of Dynamic Substructure Technology in Structural Dynamic Analysis of Launch Vehicle</a></td> </tr> </table> <table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td valign="top"><span style="line-height:22px; font-size: 15px; color:#313131">Abstract: The mass of liquid propellant has significant effects on the structural dynamics of the launch vehicle. The dynamic modeling of liquid propellant is still one of the key and difficult problems in dynamic analysis of launch vehicle.</span></td> </tr> </table></td> </tr></table><table width="100%" border="0" cellspacing="0" cellpadding="0" style=" margin-bottom:10px" height="0"> <tr> <td style="border-bottom: dotted 1px #cbcbcb;" ></td> </tr></table>]]></record> <record><![CDATA[ <table width="705" height="110" border="0" cellspacing="0" cellpadding="8" style=" margin-bottom:10px;"> <tr> <td align="left" valign="top"><table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td height="40"> <a href='/art/2015/10/8/art_1344_22139.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Study on Real-time Interactive Simulation of Rotating Top in Weightlessness</a></td> </tr> </table> <table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td valign="top"><span style="line-height:22px; font-size: 15px; color:#313131">Abstract: To solve the problems of space operation tasks training on the ground , a virtual simulation method based on human-machine interaction technology and physics engine was proposed , which successfully accomplished the virtual training of rotating top operation in weightlessness.</span></td> </tr> </table></td> </tr></table><table width="100%" border="0" cellspacing="0" cellpadding="0" style=" margin-bottom:10px" height="0"> <tr> <td style="border-bottom: dotted 1px #cbcbcb;" ></td> </tr></table>]]></record> <record><![CDATA[ <table width="705" height="110" border="0" cellspacing="0" cellpadding="8" style=" margin-bottom:10px;"> <tr> <td align="left" valign="top"><table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td height="40"> <a href='/art/2015/10/8/art_1344_22140.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Research on Application of Visional Gesture Recognition Technology in Manned Space Virtual Training</a></td> </tr> </table> <table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td valign="top"><span style="line-height:22px; font-size: 15px; color:#313131">Abstract: Aiming at the requirements of virtual assembly training for manned space missions of China， the gesture recognition technology based on Kinect was researched. A gesture detection and segmentation scheme based on depth data was proposed. Fingertips were detected through analyzing the curvature of the gesture image contour.</span></td> </tr> </table></td> </tr></table><table width="100%" border="0" cellspacing="0" cellpadding="0" style=" margin-bottom:10px" height="0"> <tr> <td style="border-bottom: dotted 1px #cbcbcb;" ></td> </tr></table>]]></record> <record><![CDATA[ <table width="705" height="110" border="0" cellspacing="0" cellpadding="8" style=" margin-bottom:10px;"> <tr> <td align="left" valign="top"><table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td height="40"> <a href='/art/2015/10/8/art_1344_22141.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Application of Virtual Prototype Technology in the Manned Space Launch Site</a></td> </tr> </table> <table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td valign="top"><span style="line-height:22px; font-size: 15px; color:#313131">Abstract: Four typical applications of virtual prototype technology in the manned space launch site were introduced，including visual modeling of key mechanical equipments，static and dynamic analysis of key mechanical structures with finite element method ( FEM )，virtual simulation and training system of electro-control equipments</span></td> </tr> </table></td> </tr></table><table width="100%" border="0" cellspacing="0" cellpadding="0" style=" margin-bottom:10px" height="0"> <tr> <td style="border-bottom: dotted 1px #cbcbcb;" ></td> </tr></table>]]></record> <record><![CDATA[ <table width="705" height="110" border="0" cellspacing="0" cellpadding="8" style=" margin-bottom:10px;"> <tr> <td align="left" valign="top"><table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td height="40"> <a href='/art/2015/10/8/art_1344_22142.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Study on Dynamic Simulationof Liquid Loop in Shenzhou Manned Spacecraft</a></td> </tr> </table> <table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td valign="top"><span style="line-height:22px; font-size: 15px; color:#313131">Abstract: In order to simulate the liquid loop in Shenzhou manned spacecraft，the models of the components were set up including the radiator，the pump，the valve，the accumulator，the cool plate and the heat-exchanger by analyzing the working principle，the flow and heat transfer performance of each components.</span></td> </tr> </table></td> </tr></table><table width="100%" border="0" cellspacing="0" cellpadding="0" style=" margin-bottom:10px" height="0"> <tr> <td style="border-bottom: dotted 1px #cbcbcb;" ></td> </tr></table>]]></record> <record><![CDATA[ <table width="705" height="110" border="0" cellspacing="0" cellpadding="8" style=" margin-bottom:10px;"> <tr> <td align="left" valign="top"><table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td height="40"> <a href='/art/2015/10/8/art_1344_22143.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Research on Global Performance Design Method of Blast Deflector in Rocket Launch Site</a></td> </tr> </table> <table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td valign="top"><span style="line-height:22px; font-size: 15px; color:#313131">Abstract: Blast deflector is one of the key infrastructures in the rocket launch site which deflects the high temperature and high pressure jet emitted by the rocket engine. Based on the computational fluid dynamics theory，theoretical analysis，experimental investigations and numerical simulation were adopted to study the launch environment effects</span></td> </tr> </table></td> </tr></table><table width="100%" border="0" cellspacing="0" cellpadding="0" style=" margin-bottom:10px" height="0"> <tr> <td style="border-bottom: dotted 1px #cbcbcb;" ></td> </tr></table>]]></record> <record><![CDATA[ <table width="705" height="110" border="0" cellspacing="0" cellpadding="8" style=" margin-bottom:10px;"> <tr> <td align="left" valign="top"><table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td height="40"> <a href='/art/2015/10/8/art_1344_22145.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Key Technology Review of the Research on the Space Station Manipulator</a></td> </tr> </table> <table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td valign="top"><span style="line-height:22px; font-size: 15px; color:#313131">Abstract: The space station manipulator of China takes on the tasks of relocking spacecraft sections ，docking assistance，installing equipments，and maintenance of the space station. It has the features of a high degree of accuracy，reliability and load ability.</span></td> </tr> </table></td> </tr></table><table width="100%" border="0" cellspacing="0" cellpadding="0" style=" margin-bottom:10px" height="0"> <tr> <td style="border-bottom: dotted 1px #cbcbcb;" ></td> </tr></table>]]></record> <record><![CDATA[ <table width="705" height="110" border="0" cellspacing="0" cellpadding="8" style=" margin-bottom:10px;"> <tr> <td align="left" valign="top"><table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td height="40"> <a href='/art/2015/10/8/art_1344_22146.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Analysis of International Space Station Payload Integration</a></td> </tr> </table> <table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td valign="top"><span style="line-height:22px; font-size: 15px; color:#313131">Abstract: For PDs and Pls’ payload integration，ISS develops two templates. One is the standard integration template and the other is the lean integration template. It is proved that they are reasonable and effective for the process of ISS payload planning，integration and operations.</span></td> </tr> </table></td> </tr></table><table width="100%" border="0" cellspacing="0" cellpadding="0" style=" margin-bottom:10px" height="0"> <tr> <td style="border-bottom: dotted 1px #cbcbcb;" ></td> </tr></table>]]></record> <record><![CDATA[ <table width="705" height="110" border="0" cellspacing="0" cellpadding="8" style=" margin-bottom:10px;"> <tr> <td align="left" valign="top"><table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td height="40"> <a href='/art/2015/10/8/art_1344_22147.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Discussion on Quantification Risk: Assessment of Chinese Manned Space Station</a></td> </tr> </table> <table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td valign="top"><span style="line-height:22px; font-size: 15px; color:#313131">Abstract: To adapt to the new characteristics of manned space missions in China and to effectively support the quantitative risk assessment for the Chinese space station，the Probabilistic Risk Assessment (PRA) work of National Aeronautics and Space Administration ( NASA) was surveyed and PRA application demonstration in different types of manned space programs</span></td> </tr> </table></td> </tr></table><table width="100%" border="0" cellspacing="0" cellpadding="0" style=" margin-bottom:10px" height="0"> <tr> <td style="border-bottom: dotted 1px #cbcbcb;" ></td> </tr></table>]]></record> </recordset> </datastore>