Method for correcting the flight path of ballistically fired...

Details Method for correcting the flight path of ballistically fired... Method for correcting the flight path of ballistically fired...

2007-09-11

2007-09-11

Swiatek, Rob (Department: 3643)

Aeronautics and astronautics

Missile stabilization or trajectory control

Externally mounted stabilizing appendage

C102S490000

Reexamination Certificate

active

10484486

ABSTRACT:
At very low apparatus expenditure, namely with a canard system which is adjustable in a single-axis mode, it is possible to achieve a spatially two-dimensional trajectory correction in respect of the artillery ammunition which in itself is unguided, with the additional degree of freedom in respect of trajectory extension and thus an extraordinary increase in the precision of delivery in relation to the predetermined target point.

REFERENCES:
patent: 4438893 (1984-03-01), Sands et al.
patent: 4964593 (1990-10-01), Kranz
patent: 5322243 (1994-06-01), Stoy
patent: 5393012 (1995-02-01), Dunn
patent: 5467940 (1995-11-01), Steuer
patent: 43 25 218 (1993-07-01), None
patent: 198 45 611 (1998-10-01), None

Affiliated with

Also associated with

Rating

Method for correcting the flight path of ballistically fired... does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Method for correcting the flight path of ballistically fired..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Method for correcting the flight path of ballistically fired... will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-3741497