首页> 外文会议>52nd International Astronautical Congress Oct 1-5, 2001 Toulouse, France >TEN CENTIMETERS ORBITS IN REAL-TIME ON-BOARD OF A SATELLITE DORIS-DIODE CURRENT STATUS
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TEN CENTIMETERS ORBITS IN REAL-TIME ON-BOARD OF A SATELLITE DORIS-DIODE CURRENT STATUS

机译:卫星DORIS-DIODE电流状态实时机载的10厘米轨道

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The DORIS system has been developped to provide high accuracy orbit determination and beacon positioning. It is fully operationnal and has been working for 10 years with Spot-2, Spot-3, Spot-4 and Topex-Poseidon. This uplink radio-electrical system is based upon precise doppler measurements (0.3 mm/s) made with the dual-frequency signals emitted by the 50 autonomous beacons distributed homogeneously over the Earth surface. The DORIS Control Center performs system monitoring (on board receivers and ground beacons), receivers programming, data processing and archive. On board gathering of the measurements allows a precise on board autonomous real-time computation of the orbit. Experienced on board of Spot-4 since 1998, DIODE (the Navigation software) has demonstrated that on-board real-time orbits are now feasible with a few meters accuracy and an availability better than 99% over 3 years, even through manoeuvers. Today, Earth observation missions, altimetry, oceanography, imaging, ..., and satellite constellations navigation often ask for a real time on board orbit restitution with a 1 meter accuracy, or even better. Including an extended force model (40x40 Earth gravitationnal fields, moon&sun attractions, ...), the last issue of DIODE is able to compute the orbit in real-time on board of the satellite, with an expected accuracy of 10 centimeters RMS on the radial component. To be launched in 2001, Envisat-1 and Jason-1 are both equipped with a DORIS 2nd generation receiver: unfortunately, flight results will not be available in time to be presented in the paper. Future flights will occur in the next years (Spot-5, Cryosat, Pleiades, ...).
机译:已经开发出DORIS系统,以提供高精度的轨道确定和信标定位。它是完全可操作的,已经与Spot-2,Spot-3,Spot-4和Topex-Poseidon合作了10年。该上行无线电系统基于精确的多普勒测量(0.3毫米/秒),该测量是利用均匀分布在地球表面的50个自治信标发出的双频信号进行的。 DORIS控制中心执行系统监视(在接收器和地面信标上),接收器编程,数据处理和存档。机载测量值的收集可实现精确的机载自主实时轨道计算。自1998年以来,DIODE(导航软件)就在Spot-4飞机上经历了丰富的经验,它证明了车载实时轨道现已可行,精度达到了几米,并且即使通过操纵,在3年内的可用性也超过了99%。如今,对地观测任务,测高,海洋学,成像等……和卫星星座导航经常要求以1米甚至更高的精度进行实时的轨道复原。包括扩展的力模型(40x40地球引力场,月球和太阳景点等),DIODE的最新一期能够在卫星上实时计算轨道,预期在卫星上的精度为10厘米RMS。径向分量。 Envisat-1和Jason-1将于2001年发射,都配备了DORIS第二代接收器:不幸的是,无法及时获得飞行结果,无法在本文中介绍。未来的航班将在未来几年内发生(Spot-5,Cryosat,Pleiades等)。

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