Advanced Sensors and Microsystems
Director
Honeywell Jun 2004 - Jun 2006
Director, Ip Commercialization
Honeywell Jan 2002 - Jun 2004
Director, Licensing
Honeywell Laboratories Jan 2000 - Jan 2002
Director, Intellectual Property Management and Licensing
Honeywell Technology Center Jan 1995 - Jan 2000
Research Section Manager
Education:
Institute of Technology, University of Minnesota 1988
Masters, Electrical Engineering
University of Minnesota 1977 - 1979
Bachelors, Bachelor of Science, Physics
Caltech 1975 - 1977
Skills:
Scientists Technology Research Solutions Engineering Automation
A noninvasive pulsed fluorescence gas velocimeter that determines dynamic parameters of a gas flow from detection of fluorescent re-radiation of excited molecules of the gas. The present invention has higher altitude capability than devices that utilize particulate scattering. The velocimeter requires no probes and utilizes a laser or other light source that does not perturb the gas flow being measured.
The United States of America as represented by the Secretary of the Air Force - Washington DC
International Classification:
F42B 1500
US Classification:
244 315
Abstract:
An electronic tripod technique for postlaunch alignment of the roll and pitch gyros of a missile inertial guidance system. Prior to launch, missile gyros are spun up and caged to the missile airframe axes. At launch, gyros are uncaged and slant range to ground measured over an azimuthal sweep symmetrical to the plane of the missile's roll and yaw axes. A roll error signal proportional to the difference between the slant ranges at the sweep extremes is generated and used to torque the roll gyro, resulting in a rotation of the missile about its roll axis until the error signal is zero. This establishes a new roll reference at the roll gyro that is normal to the local vertical. A pitch error signal is then generated that is proportional to the difference between the slant range at either sweep extreme and the slant range at 0. degree. aximuth. Similarly, this signal is used to torque the pitch gyro and establish a new pitch reference normal to the local vertical, thus completing the alignment of the roll and pitch gyros to the local vertical.
Apparatus And Method To Detect And Avoid Particles
- Morris Plains NJ, US Kenneth R. Jongsma - Tijeras NM, US Earl Thomas Benser - Chisago City MN, US Chris McKenna - Glendale AZ, US
International Classification:
G05D 1/02 G01S 13/95 G01S 7/00
Abstract:
A vehicle system is provided. The vehicle system comprises a weather sensor to provide long-range weather information, including the presence of large particles, where such long-range weather information is configured to be stored in a three dimensional volumetric representation, from which a two dimensional display and hazard information can be derived; a particle sensor to provide short-range weather information about the presence of small and large particles, wherein the particle sensor is able to differentiate between different types and sizes of particles; and at least one user interface configured to communicate weather information derived from the weather sensor and particle sensor.