Guidance computer

Boots – shoes – and leggings

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Details

364457, 364453, 367 89, G06F 1514

Patent

active

044059850

ABSTRACT:
A digital computer for guiding the flight of a ballistic missile through instrumentation of a Q Matrix. The computer may be described as being the digital counterpart of a mechanical differential analyzer in that it is made up of a number of appropriately interconnected integrators which generate the solution of the particular equation or set of equations being solved. An initial value of velocity-to-be-gained is inserted into the computer and then by means of accelerometer outputs, multipliers, adders and integrators, samples of the missile's velocity are compared with the velocity-to-be-gained to generate output signals to control or guide the trajectory of the missile during its powered flight.

REFERENCES:
patent: 2835131 (1958-05-01), Vacquier
patent: 2865579 (1958-12-01), Caillette
patent: 2932467 (1960-04-01), Scorgie
patent: 2944426 (1960-07-01), Amara
patent: 3271565 (1966-09-01), Blackman

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