Guided artillery projectile with trajectory regulator

Details Guided artillery projectile with trajectory regulator Guided artillery projectile with trajectory regulator

1988-10-21

1989-11-28

Jordan, Charles T.

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

F41G 722

Patent

active

048832391

ABSTRACT:
A guided artillery projectile with a flight attitude or trajectory regulator in the autopilot of the projectile for the guidance of a transition into a gliding trajectory at the assumption of a predetermined pitch angle after the passage through the apogee of the ballistic firing trajectory.

REFERENCES:
patent: 3946968 (1976-03-01), Stallard
patent: 4111382 (1978-09-01), Kissinger
patent: 4277038 (1981-07-01), Yates et al.
patent: 4606514 (1986-08-01), Sundermeyer
patent: 4664338 (1987-05-01), Steuer et al.
patent: 4711412 (1987-12-01), Wallermann
patent: 4840328 (1989-06-01), Sundermeyer
Isermann, Rolf; Digital Control Systems; Chapters 22-24, 1981.
Lachmann, Karl-Heinz; Parameteradaptive Regelalgorithmen fur bestimmte Klassen nichtlinearer Prozesse mit eindentigen Nichtlinearitaten, pp. 28-33.

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