Inertial navigation equations are developed which use area navigation (RNAV) waypoints and runway references as coodinate centers. The formulation is designed for aided inertial navigation systems and gives a high numerical accuracy through all phases of flight. A new formulation of the error equations for inertial navigation systems is also presented. This new formulation reduces numerical calculations in the use of Kalman filters for aided inertial navigation systems. (Author)
New Mechanization Equations for Aided Inertial Navigation Systems
1973
59 pages
Report
No indication
English
IEEE | 1986
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