Hypersonic entry vehicle state estimation using nonlinearity-based adaptive cubature Kalman filters.

Autor: Sun, Tao1 tspg5@mail.mizzou.edu, Xin, Ming1 xin@missouri.edu
Zdroj: Acta Astronautica. May2017, Vol. 134, p221-230. 10p.
Databáze: Academic Search Ultimate
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