Inertial guidance system for vertically launched missiles withou

Details Inertial guidance system for vertically launched missiles withou Inertial guidance system for vertically launched missiles withou

1978-05-25

1979-11-06

Smith, Jerry

Boots, shoes, and leggings

244 32, G06F 1550

Patent

active

041737857

ABSTRACT:
An electronic guidance system which when provided with a set of target poion coordinates prior to launch, calculates the missile position and velocity in an inertially fixed coordinate system during flight. All inertial coordinate system variables are defined by a three axis orthorganal coordinate system centered on the target position. This guidance system functions without an active roll control by continuously pointing the velocity vector of the missile towards the target position.

REFERENCES:
patent: 3198940 (1965-08-01), Loper et al.
patent: 3693909 (1972-09-01), Hall
patent: 3746281 (1973-07-01), Stripling
patent: 3924824 (1975-12-01), Brodie et al.
patent: 4038527 (1977-07-01), Brodie et al.
patent: 4123019 (1978-10-01), Amberntson

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