Method and apparatus of integrating Global Positioning System an

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364434, 244176, G06F 1550

Patent

active

051930641

ABSTRACT:
A method and arrangement for integrating a Global Positioning System and an Inertial Navigating System without the use of accelerometers to provided a velocity steering signal that is utilized in the guidance of a flying vehicle, such as a space craft. The method and arrangement do not require the use of accelerometers. A mechanization for interfacing the integrated Global Positioning System and the Inertial Navigating System with a flight control system which controls a flying vehicle is disclosed.

REFERENCES:
patent: 4402049 (1983-08-01), Gray
patent: 4405986 (1983-09-01), Gray
patent: 4894655 (1990-01-01), Joguet et al.
patent: 4899285 (1990-02-01), Nakayama et al.
patent: 4903212 (1990-02-01), Yokouchi et al.

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