Innoveering, LLC

General Electric Company

Alliant Techsystems Inc.

Orbital Atk, Inc.

George Papadopoulos

Daniel Bivolaru

Jiaji Lin

Derek R DeVries

Nicholas Tiliakos

Charles L Weigel

Charles L Dedon

Steven W Thomas

Timothy J Van Dixhorn

Clint D Thomson

Gabriel Benel

A shock wave detection system includes an optical sensor configured to generate a sensor signal based on the received laser light, a processor, and a memory. The memory includes instructions stored thereon, which when executed by the processor cause the system to: generate a sensor signal based on the laser light; perform a digital fast Fourier transform on the sensor signal; determine a power spectral density of the sensor signal based on the digital fast Fourier transform; determine a difference in a frequency content before, during, and after a shock wave transition event based on the power spectral density; and determine a passing of the shock wave based on the difference in the frequency content.

Shock wave detection systems and methods

A fluid properties sensing system includes an optical sensor which generates a sensor signal based on received laser light, a light source which transmits laser light through a transmitting fiber to a sensor head, a receiver that detects a portion of the laser light from a receiving fiber through an evanescent field of the transmitting fiber when the laser light radiates through a transmitting fiber wall of the transmitting fiber and interacts with a fluid medium at an interface of the sensor and the fluid medium, and a processor. The fibers are coupled at one end through the evanescent field to form the sensor head disposed in a flow field and to interact with the fluid medium. The processor identifies a change in the sensor signal based on a detected portion of the laser light resulting from an interaction of the sensor head with the fluid medium.

Evanescent field coupled shock wave detection systems and methods

This disclosure relates to systems and methods element identification and quantification. The method includes generating pulsed plasma based on an input voltage and a current so that the pulsed plasma interacts with a particle and atomizes the particle when the pulsed plasma is disposed in a flow field, identifying an atomic emission of the pulsed plasma with an optical sensor, determining element identification and quantification based on the identified emission of pulsed plasma, generating DC plasma having an electrical field based on an input DC voltage and a DC current, positioning the DC plasma in a flow field, detecting a change in the electrical field of the DC plasma, and determining a size of the particle based on the change in electrical field.

Plasma-based electro-optical sensing and methods

This disclosure relates to systems and methods detecting a change in pressure, wall shear flow, or both. The method includes generating DC plasma having an electrical field based on an input DC voltage and a DC current, detecting changes to the electrical field, and identifying a change in wall shear flow, pressure, or both based on the change in the electrical field when the DC plasma is disposed in a flow field.

A flight safety assembly onboard an aerial vehicle includes a first sensor configured to sense first information related to flight of the aerial vehicle and a second sensor configured to sense second information related to the flight of the aerial vehicle. A sensor input is adapted to receive third information related to the flight of the aerial vehicle. A processor is operably coupled to the first sensor, the second sensor, and the sensor input. The processor is configured to determine three independent instantaneous impact points for the aerial vehicle by independently analyzing each of the first information, the second information and the third information. The processor is also configured to generate three independent onboard flight termination indicators for each of the three independent instantaneous impact points that intersects with a region to be protected.

Methods and apparatuses for autonomous flight termination

An optical sensor comprising a light source; a sensor substrate, arranged to receive a force to be detected, the sensor substrate including an interference pattern generator, optically coupled to the light source for receiving light from the light source, and generating an interference pattern, and a detector, optically coupled to the sensor substrate for receiving the interference pattern and providing a signal which can be used to determine the force applied to the sensor substrate.

Optical coupled sensors for harsh environments

A non-intrusive sensor for in-situ measurement of recession rate of heat shield ablatives. An ultrasonic wave source is carried in the housing. A microphone is also carried in the housing, for collecting the reflected ultrasonic waves from an interface surface of the ablative material. A time phasing control circuit is also included for time-phasing the ultrasonic wave source so that the waves reflected from the interface surface of the ablative material focus on the microphone, to maximize the acoustic pressure detected by the microphone and to mitigate acoustic velocity variation effects through the material through a de-coupling process that involves a software algorithm. A software circuit for computing the location off of which the ultrasonic waves scattered to focus back at the microphone is also included, so that the recession rate of the heat shield ablative may be monitored in real-time through the scan-focus approach.

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Nesconset, NY, United States of America

George Papadopoulos