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Hybrid trajectories optimization for interplanetary missions - The MSR-ERO case

机译:截然型任务的混合轨迹优化 - MSR-ERO案例

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Thanks to its high propellant consumption efficiency, the use of electric propulsion in space missions has been constantly increasing during the last years and has been recently successfully employed also for interplanetary probes (i.e. Bepi Colombo). Nevertheless, the low-thrust capability of these propulsion systems increases considerably the transfers' duration with respect to classical chemical engines, posing serious difficulties to the realization of missions with tight timeline constraints. Shall then a mission designer mandatorily renounce either to engine efficiency or to short mission durations? The answer is no, as recently demonstrated by the Mars Sample Return (MSR) mission analysis study: for the Earth Return Orbiter (ERO) a hybrid solution, combining both chemical and electrical propulsion has been proposed, with the goal of optimizing the advantages of both systems. The overall trajectories optimization becomes in this case extremely complicated, because it combines the complexity of low-thrust trajectory optimization (such as the multi-leg interplanetary transfer or the multi-revolution spirals around Mars) with the optimal use of the chemical burns to fulfil complex timeline constraints. In this paper the work performed by DEIMOS team, as responsible of the MSR-ERO mission analysis, to optimize the hybrid ERO trajectory will be presented, with a special focus on the techniques implemented to achieve global optimum results within the real mission constraints, both at system and timeline level. All the details of a real mission design have been considered, taking into account also operational constraints such as the gravity losses for the chemical burns or the power limitation, the maximum operability time, the engine duty cycle for communication and the solar panels degradation for the electrically thrusted legs. The obtained trajectories and the distribution between chemical and electrical burns resulted to be very dependent on the specific selecte
机译:由于其高推进剂消费效率,在过去几年中,在太空任务中使用电动推进在过去几年中一直在不断增加,并且最近也已成功地用于行星际探针(即BEPI Colombo)。然而,这些推进系统的低推力能力显着增加了经典化学发动机的转移持续时间,使得具有紧密时间限制的特派团的严重困难。那么任务设计师应以发动机效率或短期使命持续发出强调?答案是否定的,正如最近由火星样本返回(MSR)任务分析研究:用于地球返回轨道(ERO)混合解决方案,结合化学和电力推进,实现了优化的优势两个系统。在这种情况下,整体轨迹优化变得非常复杂,因为它结合了低推力轨迹优化的复杂性(例如Mars周围的多腿行星际传输或多旋转螺旋),并利用化学烧伤来实现的优化使用复杂的时间轴约束。在本文中,DeiMOS团队执行的工作是展示MSR-ERO任务分析的负责,以优化混合ERO轨迹,特别关注实施在真正的任务限制内实现全球最佳结果的技术在系统和时间线级别。已经考虑了真正的任务设计的所有细节,考虑到了用于化学燃烧的重力损失或功率限制,最大可操作时间,用于通信的发动机占空比和太阳能电池板的劣化电刺腿。所获得的轨迹和化学和电气烧伤之间的分布导致非常依赖于特定的选择

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