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Modeling and Simulation of Fighter Aircraft Refueling Probe Hydraulic System Using AMESim Software

Pratik Patil1 , Prabhakar Maskar2 , Sanjay Vispute3 , Ohmkar Akhilesham4

Section:Research Paper, Product Type: Journal Paper
Volume-7 , Issue-6 , Page no. 177-181, Jun-2019

CrossRef-DOI:   https://doi.org/10.26438/ijcse/v7i6.177181

Online published on Jun 30, 2019

Copyright © Pratik Patil, Prabhakar Maskar, Sanjay Vispute, Ohmkar Akhilesham . This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

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IEEE Style Citation: Pratik Patil, Prabhakar Maskar, Sanjay Vispute, Ohmkar Akhilesham, “Modeling and Simulation of Fighter Aircraft Refueling Probe Hydraulic System Using AMESim Software,” International Journal of Computer Sciences and Engineering, Vol.7, Issue.6, pp.177-181, 2019.

MLA Style Citation: Pratik Patil, Prabhakar Maskar, Sanjay Vispute, Ohmkar Akhilesham "Modeling and Simulation of Fighter Aircraft Refueling Probe Hydraulic System Using AMESim Software." International Journal of Computer Sciences and Engineering 7.6 (2019): 177-181.

APA Style Citation: Pratik Patil, Prabhakar Maskar, Sanjay Vispute, Ohmkar Akhilesham, (2019). Modeling and Simulation of Fighter Aircraft Refueling Probe Hydraulic System Using AMESim Software. International Journal of Computer Sciences and Engineering, 7(6), 177-181.

BibTex Style Citation:
@article{Patil_2019,
author = {Pratik Patil, Prabhakar Maskar, Sanjay Vispute, Ohmkar Akhilesham},
title = {Modeling and Simulation of Fighter Aircraft Refueling Probe Hydraulic System Using AMESim Software},
journal = {International Journal of Computer Sciences and Engineering},
issue_date = {6 2019},
volume = {7},
Issue = {6},
month = {6},
year = {2019},
issn = {2347-2693},
pages = {177-181},
url = {https://www.ijcseonline.org/full_paper_view.php?paper_id=4527},
doi = {https://doi.org/10.26438/ijcse/v7i6.177181}
publisher = {IJCSE, Indore, INDIA},
}

RIS Style Citation:
TY - JOUR
DO = {https://doi.org/10.26438/ijcse/v7i6.177181}
UR - https://www.ijcseonline.org/full_paper_view.php?paper_id=4527
TI - Modeling and Simulation of Fighter Aircraft Refueling Probe Hydraulic System Using AMESim Software
T2 - International Journal of Computer Sciences and Engineering
AU - Pratik Patil, Prabhakar Maskar, Sanjay Vispute, Ohmkar Akhilesham
PY - 2019
DA - 2019/06/30
PB - IJCSE, Indore, INDIA
SP - 177-181
IS - 6
VL - 7
SN - 2347-2693
ER -

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Abstract

This paper presents the work carried out in the modeling and simulation of fighter aircraft refueling probe hydraulic system with Advanced Modeling Environment for performing Simulations of engineering systems (AMESim) as the basic platform. Various component models like axial piston pump, accumulator, bootstrap reservoir and actuators along with the influence of engine speed are modeled and integrated in the AMESim. Air to air refueling consists in transferring fuel from one aircraft to another during flight. The inputs for simulation are; engine speed, refueling actuation command, flaperon command, rudder command and other flight control surface command which are obtained from tests conducted on hydraulic system test rig for a fighter aircraft. Simulation is carried out to identify the system behaviour.

Key-Words / Index Term

AMESim, Refueling, Fighter Aircraft, Axial Piston Pump, Flight Control Surface.

References

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