公开(公告)号：US20250076000A1

公开(公告)日：2025-03-06

申请号：US18460282

申请日：2023-09-01

Applicant: BAE Systems Information and Electronic Systems Integration Inc.

Inventor： Jason H. Batchelder ,  Matthew F. Chrobak ,  Tyler Nickerson ,  Samuel C. Blauvelt

IPC: F41F3/045 ,  F41G3/16

Abstract: A portable launcher to launch a guided projectile at an aerial target, wherein the guided projectile has a projectile guidance kit and a target leading guidance kit that is provided with the guided projectile and the portable launcher. The target leading guidance kit includes a target lead estimation protocol stored on a computer readable media and accessible by a processor of the target leading guidance kit. When the processor executes the target lead estimation protocol, the processor is instructed to dynamically lead a reticle of an electronic sight of the target leading guidance kit from the initial target position to the lead target position in response to the projectile guidance kit detecting a speed of the aerial target and an inertial measurement unit of the target leading guidance kit that measures the slew of the guided projectile from the initial position to the translated position.

公开(公告)号：US20250003716A1

公开(公告)日：2025-01-02

申请号：US18344362

申请日：2023-06-29

Applicant: BAE Systems Information and Electronic Systems Integration Inc.

Inventor： Jason H. Batchelder ,  Matthew F. Chrobak ,  Tyler Nickerson ,  Richie Spitsberg

IPC: F41G7/22

Abstract: A feed forward guidance kit for a ballistic device that includes at least one optical imaging sensor, a processor that is operatively in communication with the at least one optical imaging sensor, and a feed forward guidance protocol that is stored on a computer readable medium and that is operatively in communication with the processor. When the at least one optical imaging sensor initially intercepts an aircraft at an initial location during combat, the feed forward guidance protocol instructs the processor to proactively calculate an anticipated second position of the aircraft as an orientation of the aircraft changes from an initial orientation to a translated orientation.