Measuring and testing – Navigation – Take-off and landing monitors
Patent
1979-09-24
1981-01-13
Gill, James J.
Measuring and testing
Navigation
Take-off and landing monitors
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.
Frosch Robert A. Administrator of the National Aeronautics and Space
Merhav Shmuel J.
Brekke Darrell G.
Gill James J.
Manning John R.
McMillan Armand
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