公开(公告)号：US11859956B2

公开(公告)日：2024-01-02

申请号：US17263955

申请日：2019-08-30

Applicant: BAE Systems Information and Electronic Systems Integration Inc.

Inventor： Paul Zemany ,  Matthew Chrobak

IPC: F42B15/01 ,  F42B10/14 ,  F42B10/64

CPC classification number: F42B15/01 ,  F42B10/14 ,  F42B10/64

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：US20210231425A1

公开(公告)日：2021-07-29

申请号：US17263960

申请日：2019-08-30

Applicant: BAE Systems Information and Electronic Systems Integration Inc.

Inventor： Paul Zemany ,  Matthew Chrobak ,  Egor V. Degtiarev

IPC: F42B15/01 ,  F41G7/00 ,  F41G7/34

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：US11555680B2

公开(公告)日：2023-01-17

申请号：US17263960

申请日：2019-08-30

Applicant: BAE Systems Information and Electronic Systems Integration Inc.

Inventor： Paul Zemany ,  Matthew Chrobak ,  Egor V. Degtiarev

IPC: F42B15/01 ,  F41G7/00 ,  F41G7/34

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：US20210231424A1

公开(公告)日：2021-07-29

申请号：US17263955

申请日：2019-08-30

Applicant: BAE Systems Information and Electronic Systems Integration Inc.

Inventor： Paul Zemany ,  Matthew Chrobak

IPC: F42B15/01 ,  F42B10/14 ,  F42B10/64

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.