从ETS-Ⅶ到HTV--日本交会对接/停靠技术研究  被引量:15

From ETS-Ⅶ to HTV:Study of Japanese Rendezvous and Docking/Berthing Technologies

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作  者:朱仁璋[1,2] 王鸿芳[1,3] 徐宇杰[2] 魏羽良[2] 

机构地区:[1]南京大学,南京210093 [2]北京航空航天大学,北京100191 [3]中国空间技术研究院,北京100094

出  处:《航天器工程》2011年第4期6-31,共26页Spacecraft Engineering

摘  要:日本工程试验卫星-7(ETS-Ⅶ)于1997年11月发射,成功完成在轨交会对接与空间自动机试验。ETS-Ⅶ使用GPS、激光交会雷达和邻近敏感器进行了2次V-bar与1次R-bar空间交会对接试验。空间自动机试验应用2m长的6自由度自动臂,试验项目包括卫星捕获与停靠,遥控操作,自动臂服务作业,以及卫星姿态与自动臂的协调控制。ETS-Ⅶ研发的技术在H-Ⅱ转移飞行器(HTV)飞行使命中得到应用。HTV是通往"国际空间站"的无人自动货运飞船系列,HTV-1与HTV-2分别于2009年9月与2011年1月发射。HTV执行自主R-bar逼近交会,并应用空间站遥控操作器系统进行捕获与停靠运作。空间站遥控操作器系统与日本实验舱遥控操作器系统的应用,使HTV在运送加压货物之外,还可大量运送不加压货物。HTV应用冗余技术以及诸如"故障检测、隔离与恢复"和使命中止控制的安全管理功能,可满足"1次故障保任务"和"2次故障保安全"的要求。The Japanese Engineering Test Satellite VII(ETS-Ⅶ) was launched in November 1997 to conduct the rendezvous docking(RVD) and space robot(RBT) technology experiments.Three RVD experiments(FP-1,FP-2 for V-bar approach,and FP-6 for R-bar approach) were carried out by ETS-Ⅶ,using Global Positioning System(GPS),rendezvous radar(RVR),and proximity sensor(PXS).The RBT experiments with a 2 meter-long,6 DOF manipulator arm aim at developing the technology for the space robot on an unmanned spacecraft which can be teleoperated from a ground station.The RBT experiments include capture and berthing of a target satellite as well as teleoperation,robotic servicing tasks,and coordinated control of satellite attitude and robot arm.The technologies developed through the ETS-Ⅶ project have been applied to the H-ⅡTransfer Vehicle(HTV).HTV-1 and HTV-2 were launched in September 2009 and in January 2011,respectively.HTV is an automated unmanned cargo transport system to the International Space Station(ISS),performing R-bar approach and capture-berthing with the ISS robotics arm(SSRMS).RBT technology also makes HTV have the ability to carry unpressurized cargo in addition to the pressurized cargo.As a visiting vehicle to manned ISS,HTV can meet the requirements of the one-fail operable(1FO) and two-fail safe(2FS),using redundancy technology and safety management functions such as fault detection,isolation and recovery(FDIR) and mission abort control.

关 键 词:工程试验卫星-7 H-Ⅱ转移飞行器 交会对接 停靠 自动臂 

分 类 号:V526[航空宇航科学与技术—人机与环境工程]

 

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