Autonomous navigation system

Measuring and testing – Navigation – Take-off and landing monitors

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Details

73490, 73504, G01C 2202, G01P 902

Patent

active

042442150

ABSTRACT:
An inertial navigation system utilizing a servo-controlled two-degree of freedom pendulum to obtain specific force components in the locally level coordinate system. The pendulum includes a leveling gyroscope and an azimuth gyroscope supported on a two-gimbal system. The specific force components in the locally level coordinate system are converted to components in the geographical coordinate system by means of a single Euler transformation. The standard navigation equations are solved to determine longitudinal and lateral velocities. Finally, vehicle position is determined by a further integration.

REFERENCES:
patent: 2770452 (1956-11-01), Miller
patent: 2811043 (1957-10-01), Bonnell
patent: 3071008 (1963-01-01), Steele
patent: 3077783 (1963-02-01), Stiles et al.

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