Issue2
<datastore>
<nextgroup><![CDATA[<a href="/module/jslib/jquery/jpage/dataproxy.jsp?page=1&appid=1&appid=1&webid=2&path='/'&columnid=1343&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/2015/9/30/art_1343_22120.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Study on Policies to Promote the Development of China's Manned Space Program</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: Considering the problems in the management of China's manned space program, the authors discussed how to create a more suitable major project management mode for China's national conditions, and proposed the policy suggestions on the development of China manned space program.</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/2015/9/30/art_1343_22121.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Trajectory Tracking Control and Accuracy Analysis of Space Robotic Arm Assisted Cabin Redocking</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: Cabin redocking is one of the most important tasks of the space station manipulator and high-precision tracking control during cabin transfer is a precondition for redocking. With the establishment of a high fidelity simulation model, the trajectory tracking accuracy was analyzed under different arm control and joint control strategies.</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/2015/9/30/art_1343_22122.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Failure Assessment Method for Habitable Module Structure Containing Cracks</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 existence of cracks in the structure of habitable module, which originates from the fabrication process, is inevitable. The impingement of micrometeoroid/orbital debris on the module in space may cause new crack damages to the main structure.</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/2015/9/30/art_1343_22123.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Autonomous On-orbit Health Management Architecture and Key</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 design complexity, mission diversity and the mission duration of the manned spacecraft have increased over the years, so there is an urgent need for the autonomous on-orbit health management. A hierarchical architecture where Observe-Orient-Decide-Act (OODA) loop was used to model the interaction was proposed so as to realize the precise and efficient health management.</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/2015/9/30/art_1343_22124.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Study on Impendence Control Based Target Capture Technology of Space Robotic Arm</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 the target capture of a 7-DoF Space Robotic Arm, based on the feature of contacting and impacting between the End Effector and the Target Adapter, a method of impendence control was proposed to improve the active flexible of the arm.</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/2015/9/30/art_1343_22125.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Study on Vision Measurement Technology of Space Robotic Arm</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 Robotic Arm is an indispensible key technology in maintaining the space station, performing specified tasks and ensuring the safety of EVA astronauts. The vision measurement technology is the prerequisite to complete the space teleoperation tasks with the space robotic arm.</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/2015/9/30/art_1343_22126.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Study on Design and Verification Method of Space Station Maintainability</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 highly reliable and long time operation of the space station, methods of maintainability design and on-orbit servicing are applied on the Space Station. Based on the theory and engineering practice of maintainability, the demand analysis method according to the product characteristic was discussed in this paper.</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/2015/9/30/art_1343_22127.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Analysis on Fast Spacecraft Rendezvous Technology</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: Fast rendezvous is of benefit to flight crew members and flight tasks. The basic principle is reducing of phasing revolutions. For this, a short rendezvous flight duration, within that a series of rendezvous procedure can be completed, corresponding with the smaller initial phase angle has to be designed.</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/2015/9/30/art_1343_22128.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Two-Impulse Abort Strategy for Translnnar Coast of Manned Lunar Missions Based on Artificial Immune ...</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: Abort strategy design for manned lunar missions is an important basis to ensure the safe return of the crew to Earth. First, abort strategy in different phases of manned lunar missions were analyzed based on the flight plan of Constellation program.</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/2015/9/30/art_1343_22129.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Study on International Docking System Standard</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 International Docking System Standard (IDSS) Interface Definition Document (IDD) is the result of a collaboration by the International Space Station membership to establish a recommended standard docking interface to enable on-orbit crew rescue operations and joint collaborative endeavors utilizing different spacecrafts.</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/2015/9/30/art_1343_22130.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Discussion on Some Issues of China's Space Station Safety and Mission Assurance</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 fulfill the requirements of Safety, Reliability, Maintainability, and Quality Assurance (SRM & QA) for China's space station operations, this paper summarized the advanced experience of safety and reliability on ISS based on the analysis of NASA Safety and Mission Assurance (SMA) architecture.</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/2015/9/30/art_1343_22131.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Research on TT&C System in International 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: Telemetry, Tracking and Communication ( TT&C) system is an important component of the International Space Station (ISS) . Reliable TT&C system is the foundation to ensure the long term steady operation of ISS. An in-depth comparative study on the TT&C system in ISS was conducted in this paper.</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>
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