<datastore> <nextgroup><![CDATA[<a href="/module/jslib/jquery/jpage/dataproxy.jsp?page=1&appid=1&appid=1&webid=2&path='/'&columnid=1345&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_1345_22168.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Error Analysis of Moon-to-Earth Trajectory and Choice of the First Midcourse Correction</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 error factors and their level in the flight of Moon-to-Earth trajectory were analyzed. Based on a specified Moon-to-Earth return trajectory，Monte Carlo method and statistical theory were used to quantitatively analyze the impact of the main errors on the terminals of the orbit</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_1345_22169.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Reachable Region Analysis of Orbits for Manned Lunar Landing Mission</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: Lunar global access is one of the main goals of manned lunar landing mission in the 21st century. The sunshine incidence angle and translunar orbits are the main factors influencing the lunar reachable region，although there are many others.</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_1345_22170.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Initial Alignment Calibration Off the Lunar Surface Based on Combination Navigation</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: This paper aim at the initial alignment calibration off the Lunar surface, using combination of satellite link, astronomical observation and initial device to nonlinear estate estimate, then achieve high precision position of Lunar lander, and using position information to correction initial navigation.</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_1345_22171.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Preliminary Concept Study on Integrated Lunar Exploration of Astronaut and Humanoid Robot</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 development of technologies involved in human-robot joint exploration including the humanoid robot， tele-operation， man-machine shared control， and ground verification were introduced.</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_1345_22172.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Comparison and Analysis of Cargo and Crew Combined Launch Mode and Separated Launch Mode in Manned L...</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: Because of the complexity of manned lunar landing mission，more factors must be considered to ensure the crew safety. In this paper，cargo and crew combined launch mode and cargo and crew separated launch mode was compared and discussed.</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_1345_22173.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Momentum Management and Disturbance Identification of Space Station Using DGCMG</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: This investigation focuses on the momentum management of a long-term orbiting space station. Firstly，the solution and its stability of Torque Equilibrium Attitude during momentum management were analyzed.</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_1345_22174.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">TV Image Simulation for Rendezvous and Docking Training of Astronauts</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 simulation of TV image used in astronaut rendezvous and docking mission training , the authors studied the exposure characteristics of vidicon camera applied in near-earth space with complex illumination environment and the perception characteristics of human vision</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_1345_22175.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Flight-Orbit Optimization of the Manned Maneuvering Unit with Improved Genetic Algorithm</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 ensure the safety of astronauts，Manned Maneuvering Unit ( MMU) must realize safe flight. Based on improved genetic algorithm，the flight-orbit of the manned maneuvering unit is studied and optimized.</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_1345_22176.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Direct On-orbit Gauging Method of Residual Propellant in 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 the rendezvous and docking mission of the manned space flight program， there is a need for a high-precision on-orbit gauging method on the residual propellant in the manned space-craft.</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_1345_22177.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Fusing Characteristics of Micro Tubular Fuse in High Voltage and Vacuum Environment</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 FM08 series fuses were found to exhibit sustained arcing in Vacuum Environment. RSG-I-FFA series fuses produced in China were used to study the fusing characteristics in the same situation.</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_1345_22178.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Design and Implementation of WiFi Headset in Manned Spaceflight</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: Space station wireless local area network is an important part of the space station network. WiFi headset is an important application of voice communication over space station wireless local area network，which can provide convenient wireless voice communication for IVA and EVA astronauts.</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_1345_22179.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Study on New Support Mode of Maritime Emergency Search and Rescue in Space Station Project</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: Spaceship launch will be more intensive than ever when entering into the manned space station stage，and maritime emergency search and rescue (S&R) during the ascend phase will confront sever challenges.</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>