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GEOSAT follow-on GFO radar altimeter satellite performance

机译:GEOSAT后续GFO雷达高度计卫星性能

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Under a Navy Contract with Ball Aerospace and Technologies Corporation, the first GFO satellite was completed in 1997 and launched on 10 February 1998 on an Orbital Taurus launch vehicle. The satellite was operationally accepted on 29 November 2000. With an anticipated 8-year or more life, GFO (http://gfo.bmpcoe.org/Gfo) is a DoD satellite mission managed by the PEO C4I and Space, Meteorological and Oceanographic (METOC) Systems Program Office (PMW 155) located in San Diego, California. The satellite is in the same Exact Repeat Orbit (ERO) as the original GEOSAT (800 km by 108 degrees inclination). All GFO's data products are available to the scientific community and are distributed by NOAA's Laboratory for Satellite Altimetry. The primary program objective was to develop an operational series of radar altimeter satellites to maintain continuous ocean observation for accurate global measurements of both mesoscale and basin-scale oceanography. Since its acceptance, Computer Sciences Corporation (CSC), under contract with the Navy, has provided a team known as the GFO Calibration and Validation (Cal/Val). This team, assisted by NASA and NOAA personnel, has undertaken extensive and continuing calibration and validation activities on an exact repeat cycle basis. This paper will discuss the results of those Cal/Val efforts and present charts showing the performance history of the satellite, its sensors (both the Radar Altimeter and the Water Vapor Radiometer), and other relevant performance measures such as orbit accuracy.
机译:第一个GFO卫星在1997年完成了GFO卫星的海军合同下,于1997年完成,并于1998年2月10日在轨道金牛座发射车上推出。卫星在2000年11月29日开始运作。预期的8年或更长的生命,GFO(http://gfo.bmpcoe.org/gfo)是由PEO C4i和空间,气象和海洋学管理的国防部卫星特派团(MEDOC)系统计划办公室(PMW 155)位于加利福尼亚州圣地亚哥。卫星与原始地岩浆的相同精确的重复轨道(ERO)(乘以108 km倾斜)。所有GFO的数据产品都可以向科学界提供,并由Noaa的卫星Altimetry实验室分发。主要方案目标是开发一系列雷达高度仪卫星的运营系列,以保持连续的海洋观察,以便准确全球测量Mescle和盆地海洋学。自收纳以来,计算机科学公司(CSC)与海军合同,为称为GFO校准和验证(CAL / VAL)的团队。该团队由美国宇航局和Noaa人员提供协助,并以确切的重复循环为基础进行广泛和持续的校准和验证活动。本文将讨论那些CAL / VAL努力的结果和现有图表,显示卫星的性能历史,其传感器(雷达高度计和水蒸汽辐射计)以及其他相关性能措施,如轨道精度。

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