公开(公告)号：WO2020112194A2

公开(公告)日：2020-06-04

申请号：PCT/US2019/048993

申请日：2019-08-30

Applicant: BAE SYSTEMS INFORMATION AND ELECTRONIC SYSTEMS INTEGRATION INC.

Inventor： ZEMANY, Paul D. ,  CHROBAK, Matthew F.

IPC: F42B15/10

Abstract: A guided projectile including a precision guidance munition assembly utilizes at least one maneuver envelope to optimally control movement of at least one canard to steer the guided projectile during flight. The maneuver envelopes optimize movements of the at least one canard that effectuate movement in either the range direction or the cross-range direction, or both. The maneuver envelope enables optimal timing such that maneuvering in one direction does not come at the expense of maneuver authority in the other direction.

公开(公告)号：WO2020047364A1

公开(公告)日：2020-03-05

申请号：PCT/US2019/048979

申请日：2019-08-30

Applicant: BAE SYSTEMS INFORMATION AND ELECTRONIC SYSTEMS INTEGRATION INC.

Inventor： ZEMANY, Paul D. ,  CHROBAK, Matthew F.

IPC: F41G7/00 ,  F41G7/20 ,  F41G7/22 ,  F41G7/30 ,  F41G7/34

Abstract: A system and method to aid in guidance, navigation and control of a guided projectile including a precision guidance munition assembly. The system and method receive position estimates of the guided projectile from a guiding sensor, determine predicted impact points of the guided projectile relative to a target based on the position estimates, determine miss distances of the guided projectile relative to the target, determine smoothed miss distances based, at least in part, on the determined miss distances, and process updated steering commands to steer the guided projectile based on the smoothed miss distances.

公开(公告)号：WO2020112194A3

公开(公告)日：2020-06-04

申请号：PCT/US2019/048993

申请日：2019-08-30

Applicant: BAE SYSTEMS INFORMATION AND ELECTRONIC SYSTEMS INTEGRATION INC.

Inventor： ZEMANY, Paul D. ,  CHROBAK, Matthew F.

IPC: F41G7/00 ,  F41G9/00

Abstract: A guided projectile including a precision guidance munition assembly utilizes at least one maneuver envelope to optimally control movement of at least one canard to steer the guided projectile during flight. The maneuver envelopes optimize movements of the at least one canard that effectuate movement in either the range direction or the cross-range direction, or both. The maneuver envelope enables optimal timing such that maneuvering in one direction does not come at the expense of maneuver authority in the other direction.

公开(公告)号：WO2020047383A1

公开(公告)日：2020-03-05

申请号：PCT/US2019/049013

申请日：2019-08-30

Applicant: BAE SYSTEMS INFORMATION AND ELECTRONIC SYSTEMS INTEGRATION INC.

Inventor： ZEMANY, Paul D. ,  CHROBAK, Matthew, F. ,  DEGTIAREV, Egor V.

IPC: F41G7/00 ,  F42B15/00

Abstract: A guided projectile including a precision guidance munition assembly utilizes at least one maneuver envelope to optimally control movement of at least one canard to steer the guided projectile during flight. The maneuver envelopes optimize movements of the at least one canard that effectuate movement in either the range direction or the cross-range direction, or both. The maneuver envelope enables optimal timing such that maneuvering in one direction does not come at the expense of maneuver authority in the other direction.

公开(公告)号：EP4327405A1

公开(公告)日：2024-02-28

申请号：EP22792305.9

申请日：2022-04-19

Applicant: BAE SYSTEMS Information and Electronic Systems Integration, Inc.

Inventor： ROSSMAN, Court E. ,  AFFLECK, Maxwell L. ,  CHROBAK, Matthew F. ,  FUNG, James F. ,  ZEMANY, Paul D.

IPC: H01Q1/28 ,  H01Q21/08