首页> 外文会议>Annual AAS Rocky Mountain Guidance and Control Conference; 20050205-09; Breckenridge,CO(US) >SMART-1 STAR TRACKER IRRADIATION EXPERIENCE AND BENEFITS FOR FUTURE GEOSTATIONARY TRANSFER ORBIT MYRIADE MISSIONS
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SMART-1 STAR TRACKER IRRADIATION EXPERIENCE AND BENEFITS FOR FUTURE GEOSTATIONARY TRANSFER ORBIT MYRIADE MISSIONS

机译:未来地球静止转移轨道卫星任务的SMART-1星跟踪器辐照经验和好处

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The ESA's SMART-1 mission to the Moon uses a shielded version of the highly advanced and autonomous Star Tracker (STR) "Advanced Stellar Compass (ASC)" developed by the Technical University of Denmark (DTU). SMART-1 was launched by an ARIANE 5 the September 23rd 2003. Its unique propulsion means to transit from the initial Geostationary Transfer Orbit (GTO) up to a low Lunar orbit is an ion-motor. Its perigee altitude raises from 656 km to 13,600 km within 3 months. Therefore, during that period, the equipment of SMART-1 was subjected twice per orbit to Van Allen belts radiation. Incidentally, several huge solar storms occurred within the same period. Consequently, bright spots appeared on the STR CCD and resulted in transient loss of attitude determination. Dedicated morphological filters were designed by DTU and loaded in the STR software permitting to recover to normal performance. This experience provided DTU with high heritage on the use of STR within radiation belts. The ASC also provides attitude measurement on the Low Earth Orbit MYRIADE platform developed by the French space agency: CNES. Spacecrafts based on this micro-sat platform can be launched together with 2 Geocom satellites on the ARIANE 5 launcher. So the DTU ability to work within radiation belts gives the opportunity to design and study a low cost scientific mission on GTO. To estimate the ASC capability to operate on a 2 years GTO mission, DTU has developed a model of temporal evolution of the number of hotspots on the STR CCD. Both for "permanent" and "transient" hotspots, pixel pattern and luminosity have been determined according to the CCD temperature. Using this model, it has been possible to conduct a high fidelity GTO representative test on the ALCATEL STR optical stimulator test bench. The test results demonstrate a very good robustness capability for CCD temperature up to 5℃, even at end-of-life conditions across the proton belts.
机译:ESA的SMART-1登月任务使用了由丹麦技术大学(DTU)开发的高度先进且自主的星际追踪器(STR)“高级恒星罗盘(ASC)”的屏蔽版。 SMART-1由ARIANE 5于2003年9月23日发射。其独特的推进方式是从最初的对地静止转移轨道(GTO)过渡到月球低轨道,这是一种离子电机。它的近地点高度在3个月内从656公里增加到13,600公里。因此,在此期间,SMART-1的设备在每个轨道上两次受到Van Allen带辐射。顺便说一下,在同一时期内发生了几次大的太阳风暴。因此,STR CCD上出现亮点,并导致姿态确定的短暂损失。专用形态过滤器由DTU设计,并加载到STR软件中,可恢复到正常性能。这项经验使DTU在辐射带中使用STR具有很高的传统。 ASC还可以在法国航天局CNES开发的近地轨道MYRIADE平台上提供姿态测量。基于该微卫星平台的航天器可以与ARIANE 5发射器上的2颗Geocom卫星一起发射。因此,DTU在辐射带内工作的能力为设计和研究有关GTO的低成本科学任务提供了机会。为了估算ASC执行2年GTO任务的能力,DTU开发了STR CCD上热点数量随时间变化的模型。对于“永久性”和“瞬态”热点,均已根据CCD温度确定了像素模式和亮度。使用此模型,可以在ALCATEL STR光学刺激器测试台上进行高保真GTO代表性测试。测试结果表明,即使在整个质子带寿命终止的情况下,对于高达5℃的CCD温度也具有很好的鲁棒性。

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