Open AccessDesign and Analysis of Avionic Structures For Aircraft Applications
Author(s) -
P H J Venkatesh,
M S R Viswanath
Publication year - 2020
Publication title -
international journal of modern trends in science and technology
Language(s) - English
Resource type - Journals
ISSN - 2455-3778
DOI - 10.46501/ijmtst060513
Subject(s) - avionics , modal analysis , engineering , enclosure , inertial navigation system , inertial measurement unit , software , spacecraft , global positioning system , finite element method , computer science , automotive engineering , aerospace engineering , structural engineering , inertial frame of reference , electrical engineering , telecommunications , operating system , physics , quantum mechanics
The Avionic enclosure is a electronic packed setup which are used in aircrafts and spacecrafts. Avionicenclosure is used for mechanical support to all the system elements and this is mechanically interfaced withthe aircrafts. The avionic enclosures is a key role for the system performance. The avionic package has to bedesigned to withstand high dynamics. FINGS(FIBRE OPTIC GYRO BASED INERTIAL NAVIGATION SYSTEM)is a unit of aircraft for finding the navigation. In this paper the FINGS + GPS SYSTEM (FINGS) unit designedusing SOLID WORKS and The Modal Analysis on these parts was carried out using ABAQUS FEA softwareand a random vibration experimental analysis is tested under both static and dynamic analysis. Theobtained results are compared other for the design optimization of FINGS package.