scholarly journals Functional requirements of the nuclear subsystem portions of a flight data acquisition system for nuclear modules

1967 ◽  
Author(s):  
C.E. Corl ◽  
M. Vuckovich ◽  
T.P. Weldon ◽  
N. Yaroshuk
Keyword(s):  
Data Acquisition ◽  
Data Acquisition System ◽  
Acquisition System ◽  
Functional Requirements ◽  
Flight Data ◽  
Nuclear Subsystem

scholarly journals Flight manoeuvring and safe flight visualization with the aid of wide-ranging scrutiny and automation software

2019 ◽  
Vol 272 ◽  
pp. 01021
Author(s):  
J V Muruga Lal Jeyan ◽  
Jency Lal ◽  
M Senthil Kumar ◽  
Arfaj Ahamed Anwar
Keyword(s):  
Data Acquisition ◽  
Data Acquisition System ◽  
Acquisition System ◽  
Display Module ◽  
Flight Data ◽  
Difficult Time ◽  
Standard Procedures ◽  
2D And 3D ◽  
The Impact ◽  
Graphical Presentation

This document guides to an efficient use of FDVCAS system. FDVCAS is a reconstruction, playback, interactive visualization tool, which collects, stores, processes, analyses and present the flight data in high fidelity graphical presentation in 2D and 3D format. It synchronizes and presents in both graphical and synthetic visual form to the extends of analysing the impact of the data on the system in 3D graphic animation. The existing process involves in capturing the data from different input sources and formats, analysing the features of the data monitoring is done manually in offline in a unsynchronized fashion, This is difficult, time consuming and requires highly skilled technical expertise as it is visualized in plain data form. The above standard procedures followed shall be integrated and automated with minimum intelligence to be built, in with the system. In order to analyse the flight data in a coherent way it is required to integrate both 2D and 3D form The proposed concept is the Development of a system with a single solution by providing data display, graphical charts and replay features with a sophisticated graphical user interface, which is super imposed on the outside window imagery. FDVCAS consists of Bypass data acquisition system, Outside Window Imagery (OWI) system with graphical analyser. Bypass data acquisition system receives data from aircraft recorder and transmits the data in engineering format to FDVCAS system. The OWI system has three main modules namely, 3D Visual module, GUI based Graphical analyser and Warning display module. The warnings and the graphical plots are super imposed on the 3D Visual.

Multiprocessor flight data acquisition system

1994 ◽  
Vol 40 (10-12) ◽  
pp. 871-874
Author(s):  
Zdenek Blazek
Keyword(s):  
Data Acquisition ◽  
Data Acquisition System ◽  
Acquisition System ◽  
Flight Data

Low-Cost Data Acquisition System with LabVIEW GUI for Real-Time Flight Data Transmission in UAVs

2020 ◽  
Vol V9 (03) ◽  
Author(s):  
Vikas A ◽  
Chiranth K ◽  
Dr. Hareesha N G ◽  
Srinivas Reddy P, Abdul Tanzeel ◽  
Keyword(s):  
Data Acquisition ◽  
Real Time ◽  
Data Transmission ◽  
Low Cost ◽  
Data Acquisition System ◽  
Cost Data ◽  
Acquisition System ◽  
Flight Data

Small parachute flight data acquisition system

1989 ◽  
Author(s):  
D. RYERSON ◽  
G. HAUSER
Keyword(s):  
Data Acquisition ◽  
Data Acquisition System ◽  
Acquisition System ◽  
Flight Data

scholarly journals Design of a Data Acquisition System for a Flying Laboratory

10.14311/14 ◽  
2000 ◽  
Vol 40 (1) ◽  
Author(s):  
M. Millar ◽  
L. Smrček
Keyword(s):  
Data Acquisition ◽  
Data Acquisition System ◽  
Aerospace Engineering ◽  
Acquisition System ◽  
Signal Conditioning ◽  
Flight Data ◽  
Design And Implementation ◽  
Effective Operation ◽  
The University ◽  
Made In

The University of Glasgow, Department of Aerospace Engineering has been in possession of a Czech manufactured Remotely Piloted Vehicle (RPV) airframe 1 since 1996. Significant modifications have been made and will continue to be made in order to render the design functional and airworthy. The name ‘Condor’ was chosen as the moniker for the new aircraft. The latest phase of these modifications is the design and implementation of the Condor’s in-flight data acquisition (DAQ) system. The paper will outline the various processes involved and decisions made in the design and implementation of a simple data acquisition system for a RPV. The requirements of the system were first identified, such as those quantities that were deemed essential to the effective operation of the RPV. For example, airspeed, angle of attack, angle of sideslip etc. and the necessary instrumentation for measuring such values chosen and the subsequent signal conditioning needed for the signals to be intelligible to the DAQ Card and computer.

scholarly journals Design of Data Acquisition System for Vehicle Driving Simulator

2021 ◽  
Vol 257 ◽  
pp. 01063
Author(s):  
Wanyou Xu ◽  
Dongsheng Wu ◽  
Lanlan Ping
Keyword(s):  
Data Acquisition ◽  
Real Time ◽  
High Speed ◽  
Driving Simulator ◽  
Data Acquisition System ◽  
Acquisition System ◽  
Functional Requirements ◽  
Time Data ◽  
Process Data ◽  
Vehicle Driving Simulator

Data acquisition systems have a direct impact on interactivity and authenticity to the car driving simulator. According to the requirements of the vehicle driving simulator to complete the multi-channel data acquisition and processing with high speed and high precision, a set of real-time data acquisition system was designed. The system uses STM32F103ZET6 chip to process data acquisition, and communicates with the host computer through serial port. The experimental results show that the designed data acquisition system has good real-time performance, high accuracy and meets the expected functional requirements.

Global Manufacturing: Reconfiguration of Machines in Addressing Changing Customer Requirement Scenarios

2009 ◽  
Vol 16-19 ◽  
pp. 15-19
Author(s):  
Michael Flowers ◽  
Kai Cheng
Keyword(s):  
Data Acquisition ◽  
Surface Topography ◽  
White Light ◽  
Manufacturing Systems ◽  
Data Acquisition System ◽  
Acquisition System ◽  
Functional Requirements ◽  
Customer Requirements ◽  
Customer Requirement ◽  
Experimental Trials

The dynamics of customer requirements in the global domain are dictating a need for the reconfiguration of existing conventional manufacturing systems in order to adapt and respond to the changing functional requirements. This study presents the investigation of the feasibility of adapting a hydraulic cam system to a power press for uphill sheetmetal piercing. The surface topography of sheared edges of blanks and slugs was analyzed using Zygo New View 200 Scanning White Light Interferometer. The piercing force in each trial was monitored and analyzed via computer-press interface data acquisition system (DAS). The average piercing force, 10721N, obtained was found to be nearly constant throughout the experimental trials.

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