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Analysis of a station-keeping maneuver strategy for three geostationary satellites collocation

机译:三颗对地静止卫星并置的驻地机动策略分析

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摘要

A collocation strategy have been planned and analyzed for three geostationary satellites in the same longitude control bo. The orbit determination error analysis is performed when only one ground station is used for the angle tracking and ranging. Based on the orbit determination errors, the station-keeing bands are allocated for 7-day East/West station-keeping maneuver cycle. The eccentricity control circle and inclination control box for individual stallite are allocated for the collocation. The eccentricity vector and inclination vector separation method is applied for the collocation, and the maneuver shedule is planned to minimize the operational load by avoiding similtaneous maneuvers. Toal of eighty days of station-keepting maneuver siulations are performed for the three collocated stellites. The nutual distances between the satellites are monitored for avoiding collisions.
机译:已经计划并分析了在同一经度控制bo中的三颗对地静止卫星的搭配策略。当仅将一个地面站用于角度跟踪和测距时,将执行轨道确定误差分析。根据轨道确定误差,为7天的东西方站位保持机动周期分配站位敏感带。并排配置了用于各个档位的偏心控制圈和倾斜度控制盒。偏心向量和倾斜向量分离方法被应用于该搭配,并且该机动皮具计划通过避免同时机动而最小化操作负荷。对三个并置的星体进行了为期80天的保持站台操纵的模拟操作。监视卫星之间的名义距离,以避免碰撞。

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