A Precise Altitude Difference Measurement System for Terrain Mapping and Application in a Ducted-Fan Powered Airplane

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F17%3A00313917" target="_blank" >RIV/68407700:21220/17:00313917 - isvavai.cz</a>

Alternative codes found

RIV/68407700:21230/17:00313917

Result on the web

<a href="http://dx.doi.org/10.1109/DASC.2017.8102109" target="_blank" >http://dx.doi.org/10.1109/DASC.2017.8102109</a>

DOI - Digital Object Identifier

<a href="http://dx.doi.org/10.1109/DASC.2017.8102109" target="_blank" >10.1109/DASC.2017.8102109</a>

Result language

angličtina

Original language name

A Precise Altitude Difference Measurement System for Terrain Mapping and Application in a Ducted-Fan Powered Airplane

Original language description

This article describes the assembly and performance of a differential pressure measurement system adapted to provide information about altitude difference. The system is being tested in different conditions and it is adapted for position angles measurement in a ducted fan-powered airplane. The main contribution of the article is a comparison of characteristics of pressure sensors suitable for differential measurement and consequently for altitude difference measurements. The proposed applications are precise large-scale terrain mapping and this article describes its usage on relatively small area given by size of the airplane that is flying at speeds higher than 100 km/h. The airplane design considerations are made to accommodate the proposed measurement system, which uses properties of standard atmosphere to determine the roll angle and the pitch angle of the airplane. We describe the details of the airplane that are necessary for the installation of the measurement system. The application on the airplane requires high precision sensors and installation. We describe the proposed principle of measurement as well as the data analysis and its performance under different conditions. These conditions include laboratory setup, UAV flight, an installation on a Cessna airplane, a stratospheric balloon and usage on a prototype of ducted fan powered airplane.

Czech name

—

Czech description

—

Type

D - Article in proceedings

CEP classification

—

OECD FORD branch

10201 - Computer sciences, information science, bioinformathics (hardware development to be 2.2, social aspect to be 5.8)

Project

<a href="/en/project/FV10505" target="_blank" >FV10505: Intelligent composite anchoring element</a><br>

Continuities

P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year

2017

Confidentiality

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection

2017 IEEE/AIAA 36th Digital Avionics Systems Conference (DASC)

ISBN

978-1-5386-0365-9

ISSN

2155-7195

e-ISSN

—

Number of pages

6

Pages from-to

—

Publisher name

IEEE

Place of publication

New York

Event location

St.Petersburg, Florida

Event date

Sep 17, 2017

Type of event by nationality

WRD - Celosvětová akce

UT code for WoS article

000417412000122