Sensors of a Beechcraft C90 Aircraft for Extension of Data Acquisition System
| Autor: | Elena BALMUS, Inken PELTZER |
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| Jazyk: | angličtina |
| Rok vydání: | 2017 |
| Předmět: | |
| Zdroj: | INCAS Bulletin, Vol 9, Iss 1, Pp 107-115 (2017) |
| Druh dokumentu: | article |
| ISSN: | 2066-8201 2247-4528 |
| DOI: | 10.13111/2066-8201.2017.9.1.11 |
| Popis: | In-flight data acquisition is a key point in the aircraft design process. For the control of a simulated prototype using the control surfaces, state variables such as acceleration, pitch rate for longitudinal motion, and roll rate or slideslip angle for lateral-directional motion are commonly defined as control variables. The purpose of this paper is to evaluate the risk of in -flight laboratory modification through extension of data acquisition system for collection of additional data related to pilot command input and the reaction of the system. |
| Databáze: | Directory of Open Access Journals |
| Externí odkaz: |
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