Is this project an undergraduate, graduate, or faculty project?

Undergraduate

Project Type

group

Campus

Daytona Beach

Authors' Class Standing

Celso Ferreira De Moura, Senior

Lead Presenter's Name

Celso Ferreira De Moura

Lead Presenter's College

DB College of Engineering

Faculty Mentor Name

Dr. Kyle Collins

Abstract

This work presents the design and implementation of a fully integrated data acquisition system for a full scale Integrated High Lift Propulsion testbed based on a Cessna 182Q, with emphasis on hardware integration, sensor reliability, and time synchronization. A centralized architecture was developed in LabVIEW to acquire, process, and store data from both analog and digital sensors, including air data systems, inertial measurement units, control positions, and propulsion instrumentation. Analog sensors were carefully calibrated to ensure accurate conversion to engineering units, while digital sensors were incorporated into a unified framework to maintain consistency across all measurements. All ADC, GPS, INS, and EDM data were logged together within this system and synchronized onto a common timeline. A key aspect of this system is the implementation of a precise time alignment method using a Pulse Per Second signal, enabling synchronization of all data streams onto a common reference timeline. This approach ensures accurate data correlation during dynamic flight maneuvers and minimizes timing discrepancies between independently sampled systems. Additional hardware considerations, such as IMU dampening, were implemented to reduce vibration induced noise and improve overall data quality. Initial flight testing demonstrated reliable system performance, consistent sensor behavior, and high quality data suitable for further analysis. The synchronized dataset supports air data system calibration and system identification efforts. Results have shown strong measurement consistency, and detailed findings will be presented.

Did this research project receive funding support (Spark, SURF, Research Abroad, Student Internal Grants, Collaborative, Climbing, or Ignite Grants) from the Office of Undergraduate Research?

No

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Design and Implementation of a Synchronized Data Acquisition System for an IHLP Cessna 182 Testbed

This work presents the design and implementation of a fully integrated data acquisition system for a full scale Integrated High Lift Propulsion testbed based on a Cessna 182Q, with emphasis on hardware integration, sensor reliability, and time synchronization. A centralized architecture was developed in LabVIEW to acquire, process, and store data from both analog and digital sensors, including air data systems, inertial measurement units, control positions, and propulsion instrumentation. Analog sensors were carefully calibrated to ensure accurate conversion to engineering units, while digital sensors were incorporated into a unified framework to maintain consistency across all measurements. All ADC, GPS, INS, and EDM data were logged together within this system and synchronized onto a common timeline. A key aspect of this system is the implementation of a precise time alignment method using a Pulse Per Second signal, enabling synchronization of all data streams onto a common reference timeline. This approach ensures accurate data correlation during dynamic flight maneuvers and minimizes timing discrepancies between independently sampled systems. Additional hardware considerations, such as IMU dampening, were implemented to reduce vibration induced noise and improve overall data quality. Initial flight testing demonstrated reliable system performance, consistent sensor behavior, and high quality data suitable for further analysis. The synchronized dataset supports air data system calibration and system identification efforts. Results have shown strong measurement consistency, and detailed findings will be presented.

 

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