Mathematical Problems in Engineering / 2012 / Article / Fig 4

Research Article

Unscented Kalman Filter Applied to the Spacecraft Attitude Estimation with Euler Angles

Figure 4

Attitude errors (Standard Deviation) estimated.
985429.fig.004a
(a)
985429.fig.004b
(b)
985429.fig.004c
(c)

Article of the Year Award: Outstanding research contributions of 2020, as selected by our Chief Editors. Read the winning articles.