发明名称 Trajectory Estimation System for an Orbiting Satellite
摘要 In one embodiment of the disclosure, a computing system includes a processor and a computer readable medium. The computer readable medium is operable to, when executed on the processor, determine an estimated trajectory of a satellite using a sequential mode of operation, perform a thruster burn, receive a data point from an uplink/downlink facility, determine an estimated trajectory and an estimated thruster performance of the satellite based upon the received data point. If the trajectory error is above a specified threshold level, repeat receiving an updated data point from the uplink/downlink facility, determining an updated estimated trajectory and an updated estimated thruster performance of the satellite based upon the updated data point, and determining an updated trajectory error based upon the updated data point.
申请公布号 US2008275598(A1) 申请公布日期 2008.11.06
申请号 US20070744059 申请日期 2007.05.03
申请人 SCHWARTZ LAWRENCE 发明人 SCHWARTZ LAWRENCE
分类号 G01C21/20;G06F7/00;G06F19/00 主分类号 G01C21/20
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