a novel navigation method used in a ballistic missile.pdf
一种新的应用于弹道导弹的惯性/天文组合导航算法被提出。该算法使用折射星导航来补偿加速度计引起的误差,并通过可观测性分析,分析了当折射星的数目多余3克的时候系统方程收敛
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