Ideal trajectory shaping for anti-armor missiles via gimbal angl

Details Ideal trajectory shaping for anti-armor missiles via gimbal angl Ideal trajectory shaping for anti-armor missiles via gimbal angl

1978-03-13

1983-05-17

Eisenzopf, Reinhard J.

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

244175, F41G 700

Patent

active

043836623

ABSTRACT:
Apparatus and method of anti-armor missile trajectory shaping for optimum rhead penetration of armor by a guided missile. The guidance system utilizes a terminal homing guidance unit in conjunction with a programmed control signal through the missile's autopilot to cause the missile to cruise at low altitudes and then dive onto the armor target. The terminal dive angle can be selected dependent upon the target's armor characteristics.

REFERENCES:
patent: 3094299 (1963-06-01), Bond et al.
patent: 3695555 (1972-10-01), Chadwick
patent: 3735944 (1973-05-01), Bannett et al.
patent: 3945588 (1976-03-01), Maglio, Jr.
patent: 4006871 (1977-02-01), Simpson
patent: 4010365 (1977-03-01), Meyers et al.
patent: 4108400 (1978-08-01), Groutage et al.
patent: 4123019 (1978-10-01), Amberntson

Affiliated with

Also associated with

Rating

Ideal trajectory shaping for anti-armor missiles via gimbal angl does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Ideal trajectory shaping for anti-armor missiles via gimbal angl, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Ideal trajectory shaping for anti-armor missiles via gimbal angl will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-1563865