Lawrence A Humm

6794987, Sep 21, 2004

Jul 1, 2002

10/186784

Jan K. Schiffmann - Newbury Park CA
Lawrence A Humm - West Hills CA

Delphi Technologies, Inc. - Troy MI

B60Q 100

340435, 340903, 340917, 701301

A collision detection system and method of estimating a miss distance of an object and estimating length and width of the object are provided. The collision detection system includes a sensor for sensing an object within a field of view and measuring range and range rate of the sensed object. The collision detection system further includes a controller for estimating a miss distance of the object and further estimating length and width of the object as a function of the range and the range rate.

8604968, Dec 10, 2013

Oct 6, 2009

13/119307

Stephen W. Alland - Newbury Park CA, US
Richard C. Lind - Noblesville IN, US
William G. Shogren - Noblesville IN, US
Lawrence A. Humm - West Hills CA, US
William A. Bauson - Zambia, ZM
Shawn Shi - Thousand Oaks CA, US

Delphi Technologies, Inc. - Troy MI

G01S 13/00

342 70, 342 22, 342 27

An integrated radar-camera sensor is provided which includes a camera sensor component and a radar sensor component both housed within a common single module housing. The sensor module also includes processing circuitry for processing the radar sensor and camera outputs. The sensor module is located behind the windshield of a vehicle and may include glare and/or EMI shields.

51180502, Jun 2, 1992

Aug 16, 1990

7/568298

Keith P. Arnold - Canoga Park CA
Lawrence A. Humm - West Hills CA
Han S. Pan - Newbury Park CA
I-Ping Yu - Thousand Oaks CA
Robert Rosen - Granada Hill CA

Hughes Aircraft Company - Los Angeles CA

F41G 728

244 314

In a weapon system 10 incorporating a target position sensor (14), an information system (16), a power source (22), a launcher (20), and an airborne vehicle (18), a launcher control system (12) which incorporates a communications interface (26) for coupling the information system (16) and the target position sensor (14) to a launcher (20) and an airborne vehicle (18). The communications interface (26) receives target position information and launch and control orders and provides launcher and airborne vehicle status. A airborne vehicle interface (28) couples the launcher (20) and the airborne vehicle (18) to the information system (16) and a power source (22). A transmitter (30) communicates updated target position information to the airborne vehicle after launch. A power control unit (32) converts and regulates power from different power sources (22) to be used by the launcher control system (12). The launcher (20) with launcher control system (12) is preferably modular in construction and is separate from the information system (16) and target position sensor (14).