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SIMULASI AIRSPEED INDICATOR MENGGUNAKAN SENSOR TEKANAN
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Institusion
INSTITUT TEKNOLOGI DIRGANTARA ADISUTJIPTO
Author
WIDABUDIATMA, WAHYU
Subject
T Technology (General) 
Datestamp
2024-08-21 04:55:38 
Abstract :
In this sophisticated era, it must be supported with sophisticated equipment as well. Lecture activities in the classroom need to be supported by practical activities related to existing theories, in order to make it easier to understand theoretical courses. Thus, many practicum equipment must be provided in a technical laboratory to support courses aimed at verification. In addition, practicum is a material for student training to observe existing problems so that they can be resolved and concluded. Designing an aircraft speed system requires an MPX5700AP pressure sensor. The web-controlled monitoring system that is operated by NodeMCU as a microcontroller and in its connectivity is assisted by wifi. This system is designed to determine the speed of flight when flying directly which is expected to help in providing information to students regarding aircraft speed data. From the results of the aircraft speed monitoring system, the MPX5700AP pressure sensor is used to detect the speed of an aircraft capable of calculating speeds from 10 Psi to 924 Psi. The error obtained is from 1.1% to 19.1%. This error is a comparison between MPX5700AP pressure sensor and GPS sensor. GPS sensor as the aircraft speed detector is only able to detect aircraft speeds from 1.69 Mph to 66.74 Mph. The magnitude of the error is caused by the difference from the respective sensor units. 
Institution Info

INSTITUT TEKNOLOGI DIRGANTARA ADISUTJIPTO