Registers – Calculators – Input-output calculator to indicator – printer – etc.
Patent
1976-06-28
1977-09-06
Gruber, Felix D.
Registers
Calculators
Input-output calculator to indicator, printer, etc.
89 15R, 235 615T, 244 14, G06G 780
Patent
active
040469930
ABSTRACT:
A system for determining the proper instant of time to launch an object, h as a target or torpedo, from an aircraft to cause the object to impact a water surface at a predetermined nose-down angle, thereby preventing structural damage due to high impact forces. The system utilizes signals produced by instrumentation representative of the aircraft pitch and angular rate of pitch. The desired launch altitude and predetermined impact angle are physically set into the system by means of adjustable voltage sources. These parameters are processed in the system such that the system forms a complete electronic analogy to the physical laws which govern the motion of the free falling object. In operation, the system continuously computes the predicted impact angle based on the instantaneous inputs of the aircraft's altitude, pitch angle and pitch rate. It then compares the predicted impact angle with the predetermined impact angle. Whenever the predicted impact angle exceeds the predetermined impact angle, a launch signal is produced to release the object.
REFERENCES:
patent: 2518916 (1950-08-01), Luck
patent: 3171324 (1965-02-01), Ernst et al.
patent: 3699310 (1972-10-01), Cole
patent: 3860791 (1975-01-01), Headle
Moran Patrick J.
Wilson Charles A.
Cochran II William W.
Gruber Felix D.
Sciascia Richard S.
St. Amand Joseph M.
The United States of America as represented by the Secretary of
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