首页> 外文会议>IAA Symposium on Small Satellite Missions;International Astronautical Congress >AN OPTIMIZATION APPROACH FOR DESIGNING OPTIMAL TRACKING CAMPAIGNS FOR LOW-RESOURCES DEEP-SPACE MISSIONS
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AN OPTIMIZATION APPROACH FOR DESIGNING OPTIMAL TRACKING CAMPAIGNS FOR LOW-RESOURCES DEEP-SPACE MISSIONS

机译:用于低资源深空任务的最佳跟踪运动的优化方法

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This work contributes to the autonomous scheduling of orbit determination campaigns for tracking spacecraft in deep-space by developing a dedicated optimisation algorithm. Given a network of available ground stations, the developed method autonomously generates optimized tracking observation campaigns, in terms of stations to use and time of measurements, which minimize the uncertainty associated to the state of the satellite. The outcome is a set of optimal solutions characterized by different allocated budgets, among which lhe operators can chose the most appropriate or promising one. The developed approach relies on a Structured-Chromosome Genetic Algorithm that copes with mixed-discrete global optimization problems with variable-size design space. This operates on a hierarchical reformulation of the problem by means of revised genetic operators. The estimation of the spacecraft state, and its uncertainty, given a set of measurements is performed using a sparse Gauss-Hermite Kalman Filter. The proposed approach has been tested to the design of observation campaigns for tracking a satellite in its interplanetary cruise to an asteroid. Uncertainty is considered in the initial conditions, execution errors and observation noises.
机译:通过开发专用优化算法,这项工作有助于通过开发专用优化算法来跟踪深空中航天器的轨道确定运动的自主调度。鉴于可用的地站网络,开发方法在使用和测量时间的站点方面自主地生成优化的跟踪观察活动,这最小化了与卫星状态相关的不确定性。结果是一系列以不同的分配预算为特征的最佳解决方案,其中LHE运营商可以选择最合适或承诺的。开发的方法依赖于结构化 - 染色体遗传算法,其与可变尺寸设计空间的混合离散全局优化问题。通过修改后的遗传算子来解决问题的分层重构。使用稀疏的高斯-Hermite Kalman滤波器来执行估计航天器状态的估计和其不确定性。已经测试了拟议的方法,以了解在其行星巡航中跟踪卫星的观察活动设计到小行星。在初始条件下考虑不确定性,执行错误和观察噪声。

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