首页> 外文会议>AAS/AIAA space flight mechanics meeting >EFFICIENT PARALLELIZATION OF NONLINEAR PERTURBATION ALGORITHMS FOR ORBIT PREDICTION WITH APPLICATIONS TO ASTEROID DEFLECTION AND FRAGMENTATION
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EFFICIENT PARALLELIZATION OF NONLINEAR PERTURBATION ALGORITHMS FOR ORBIT PREDICTION WITH APPLICATIONS TO ASTEROID DEFLECTION AND FRAGMENTATION

机译:非线性扰动算法在轨道预测中的有效并行化及其在星体偏转和破碎中的应用

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Orbit determination and control problems are sometimes solved using linearizedmethods, even though nonlinear effects can sometimes dominate the system. Thispaper addresses ways to parallelize computational algorithms for numerical integratorsand nonlinear relative motion equations. An application of the proposedmethods to mutual gravitation of a fragmented asteroid is presented, with analysisof the relative efficiency of parallel architechtures. Hydrodynamic simulationof a subsurface nuclear explosion is used to generate the initial conditions, afterwhich the fragmented system is propagated in parallel including mutual gravitationalterms. Efficient algorithms for this problem emphasize the achievement ofverifiable results for asteroid deflection/fragmentation research using limited orbudget-allocated computer resources.
机译:有时使用线性化解决轨道确定和控制问题 即使非线性效应有时可以支配整个系统,也可以采用这些方法。这 论文提出了并行化数值积分器计算算法的方法 和非线性相对运动方程。建议的应用 提出了使小行星相互引力的方法,并进行了分析 并行架构的相对效率。流体动力学模拟 地下核爆炸的爆炸被用来产生初始条件, 包括相互引力在内的碎片系统并行传播的过程 条款。针对此问题的高效算法强调了 使用有限度或有限度的小行星偏转/碎片研究的可验证结果 预算分配的计算机资源。

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