Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1971-07-26
1976-04-13
Feinberg, Samuel
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
F41G 700
Patent
active
039499545
ABSTRACT:
A projectile carrying a Loran processor is directed to a target along a line, referred to as a lorhumb line, which is the locus of all points i for which TDA- TDA.sub.i /TDB- TDB.sub.i is constant. Any deviation results in a cross-track error directing the projectile back on a correct path to the target. No vertical tracking is necessary because the projectile is flown near to the target and caused to execute a ballistic foldover so that it travels vertically downward towards the target. During vertical descent an along-path error signal is generated to control the vertical fins of the projectile.
REFERENCES:
patent: 2821349 (1958-01-01), Sohn
Ato Inc.
Feinberg Samuel
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