Measuring and testing – Navigation – Take-off and landing monitors
Patent
1977-07-22
1978-09-19
Woodiel, Donald O.
Measuring and testing
Navigation
Take-off and landing monitors
364450, 364453, G01C 2100
Patent
active
041144376
ABSTRACT:
The vehicle is operated over land which is described by a grid coordinate system having a north direction offset from geographic north. The vehicle has a pick-up to determine its heading speed along its longitudinal center line. The spin axis of a free gyro establishes a reference axis. A meridian gyro determines the angle, if any, between said reference axis and geographic north at the start of a mission. At the start of the mission a computer is supplied with information as to the starting point in said grid coordinate system, the angle between geographic north and grid north, and an estimated corrective factor (based on the type of terrain to be traversed) to be applied to the measured heading speed. The computer continuously determines, for display, the position of the vehicle in said grid system. Upon the vehicle reaching a landmark whose coordinates in said grid system are known, the correct coordinates for the then location of the vehicle are supplied to the computer and the computer determines the error in the estimated corrective factor and thus determines a revised corrective factor to be employed upon leaving said landmark.
REFERENCES:
patent: 3849636 (1974-11-01), Helms
Bodenseewerk
Woodiel Donald O.
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