G - Physics – 05 – D
Patent
G - Physics
05
D
342/2, 341/80
G05D 1/12 (2006.01) F41G 7/30 (2006.01)
Patent
CA 1041634
ABSTRACT OF THE DISCLOSURE A guidance and control system for continuously maintaining a missile along the line of sight between a ground vehicle and a ground target. A first communication link between the missile and the vehicle, including a missile source transmitting infrared energy and a vehicle tracker, continuously measures the location of the missile with respect to the line of sight, with the vehicle tracker providing yaw and pitch error signals. A guidance and control computer n the vehicle generates compensating signals proportional to missile flight time and target motion at right angles to the line of sight, and combines the compensating signals with equalized error signals to generate pitch and yaw command signals. A second communication link between the missile and the vehicle, including a vehicle transmitter for transmitting the pitch and yaw command signals and a missile receiver for receiving the command signals, provides correction signals to missile flight control means for maintaining the missile along the line of sight. The flight control means includes an equalization network for stabilizing the correction signals.
929972
Durand Eric
Smith Carl H.
Walters Louis G.
LandOfFree
Radiant energy guided missile system does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Radiant energy guided missile system, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Radiant energy guided missile system will most certainly appreciate the feedback.
Profile ID: LFCA-PAI-O-374488