公开(公告)号：WO2018190788A1

公开(公告)日：2018-10-18

申请号：PCT/US2017/026775

申请日：2017-04-10

Applicant: BAE SYSTEMS INFORMATION AND ELECTRONIC SYSTEMS INTEGRATION INC.

Inventor： SCHORR, David J ,  BATCHELDER, Jason H ,  GIBSON, Jeremy B ,  STEENSON, JR., James H

IPC: F42B10/00

Abstract: [A system and method for dynamic autopilot control comprising providing input to a guidance and control autopilot comprising Mach and dynamic pressure; tailoring parameters of the autopilot, the parameters comprising : roll gain; a pitch/yaw gain; a pitch/yaw loop compensator frequency; a guidance filter bandwidth; a guidance filter lead compensator frequency; and a navigation gain.

公开(公告)号：WO2019035834A1

公开(公告)日：2019-02-21

申请号：PCT/US2017/047276

申请日：2017-08-17

Applicant: BAE SYSTEMS INFORMATION AND ELECTRONIC SYSTEMS INTEGRATION INC.

Inventor： SCHORR, David J ,  GIBSON, Jeremy B ,  STEENSON, JR., James H

IPC: G05D1/10 ,  F41G7/22 ,  G01C21/20

Abstract: A device, system, and method for shaping the trajectory of a projectile employing a Gravity bias, Gbias. The system includes a seeker, a guidance filter, a pitch rate filter, an actuator, pitch/yaw/roll coupled aerodynamics, and lateral rate sensors. It receives roll orientation input to a guidance and control autopilot; it applies Additional Gbias to that produced by the null rate command to the lateral control loops of the guidance and control autopilot device. The lateral rate command is equal to the desired Additional Gbias divided by an estimate of the projectile velocity. The Additional Gbias is translated to a rate command and incorporated into guidance loop commands to boost an Inherent Gbias to shape the trajectory of the projectile to the target.

公开(公告)号：EP3669248A1

公开(公告)日：2020-06-24

申请号：EP17921805.2

申请日：2017-08-17

Applicant: Bae Systems Information And Electronic Systems Integration Inc.

Inventor： SCHORR, David J ,  GIBSON, Jeremy B ,  STEENSON, JR., James H

IPC: G05D1/10 ,  F41G7/22 ,  G01C21/20