Adam J Robertson

US Patent:

8576111, Nov 5, 2013

Filed:

Jun 22, 2009

Appl. No.:

12/488668

Inventors:

Ryan L. Smith - Salem UT, US
Logan C. Harris - Orem UT, US
David G. Long - Provo UT, US
Adam E. Robertson - Provo UT, US
Adam R. Harper - Provo UT, US
Britton T. Quist - Orem UT, US
Joshua M. Hintze - Austin TX, US

Assignee:

IMSAR LLC - Springville UT

International Classification:

G01S 13/90

US Classification:

342 25F, 342 75

Abstract:

A compact synthetic aperture radar system and associated methods are disclosed.

US Patent:

20210323671, Oct 21, 2021

Filed:

May 10, 2021

Appl. No.:

17/316364

Inventors:

- Pleasant Grove UT, US
Devin Donald LEBARON - Saratoga Springs UT, US
Adam Eugene ROBERTSON - Provo UT, US

International Classification:

B64D 7/06
F41A 19/59
F41B 11/80
F41B 11/62
F41H 13/00
B64C 39/02
F41B 11/723

Abstract:

A projectile component that can be removably attached to a flying vehicle is disclosed. The projectile component includes a net configured in the projectile component, a receiving cavity configured in the projectile component, and a weight attached to the net via a string. The weight can be configured in the receiving cavity in preparation for firing the net from the projectile component. In order to entangle a target flying vehicle in the net, a cocklebur associated with the weight is included. Upon firing the net from the projectile component, and upon the net engaging with a target device, the cocklebur becomes entangled with the net to secure the target flying vehicle. A drawstring structure associated with the net can also be used to ensure that the net envelops and captures the target flying vehicle.

US Patent:

20210323672, Oct 21, 2021

Filed:

May 10, 2021

Appl. No.:

17/316433

Inventors:

- Pleasant Grove UT, US
Devin Donald LEBARON - Saratoga Springs UT, US
Adam Eugene ROBERTSON - Provo UT, US

International Classification:

B64D 7/06
F41A 19/59
F41B 11/80
F41B 11/62
F41H 13/00
B64C 39/02
F41B 11/723

Abstract:

A projectile cartridge that can be removably attached to a flying vehicle is disclosed. A system can include a first flying vehicle, a projectile attachment mechanism configured with the first flying vehicle, a projectile cartridge that contains a projectile, the projectile cartridge being removably attachable to the projectile attachment mechanism, a weight attached to the projectile, the weight being configured in a releasable configuration in the projectile cartridge and a drawstring configured with the projectile. After firing the projectile, when tension is applied to the drawstring as the projectile approaches or envelops a second flying vehicle, the tension can cause the drawstring to close the projectile down to secure the second flying vehicle.

US Patent:

20200103499, Apr 2, 2020

Filed:

Oct 1, 2019

Appl. No.:

16/589678

Inventors:

- Pleasant Grove UT, US
Mikko Valimaki - Orem UT, US
Mitchell Kay Oldroyd - Bluffdale UT, US
Adam Eugene Robertson - Provo UT, US
Bryan Alan Davis - Salt Lake City UT, US
Matthew Elliott Argyle - Lindon UT, US
David Thimm - Orem UT, US
James David Mackie - Provo UT, US

International Classification:

G01S 7/41
G06N 3/04
G06N 3/08
G01S 13/86

Abstract:

A method and system device provides a unique object identification process by obtaining information from one or more of radar signals, infrared signals, optical signals, audio signals, and other signals. The method includes continuously receiving object data at the device, applying by a machine learning system, a set of parameters to process the object identification and confidence level, and outputting or updating the object identification, confidence level, and actionable recommendations. The radar data includes a Doppler signature having a wrapped signal due to a sampling rate of the radar system. The Doppler signature is used to train the machine learning system to identify drone types.