PaperAAIAA Journal3/23/2026Spacecraft Attitude Determination System Based on the Sequential Solution of the Two Inverse ProblemsEvgenii V. Chebakov·Dmitry M. Titov·Aleksey V. Nenarokomov·Dmitry L. Reviznikov·Sergey A. BudnikRead at AIAA JournalShareLess like thisTagsInertial Sensor and NavigationAerospace Engineering
