Method and arrangement for determining passage through an apogee

Details Method and arrangement for determining passage through an apogee Method and arrangement for determining passage through an apogee

1988-05-09

1989-08-15

Jordan, Charles T.

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

F41G 700

Patent

active

048567337

ABSTRACT:
A method for the on board determination for the passage through an apogee by a ballistically launched projectile through the receipt and comparison of a sequence of measured values vacillating or fluctuating specifically relative to the trajectory. Also disclosed is an arrangement for the on board determination of the point in time of an apogee of a projectile which is launched in a ballistic trajectory, through the receipt and comparison of a sequence of measured values vacillating specific to the trajectory.

REFERENCES:
patent: 3332642 (1967-07-01), Halling
patent: 4606514 (1986-08-01), Sundermeyer
Chapters 1 and 4 of "Parameteradaptive Regelalogorithmen fur bestimmte Klassen nincht-linearer Prozesse mit eindeutigen Nichtlinearitaten" (Progress Reports from the VDI-Journals, Series 8, No. 66, 1983).

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