SIMULASI KENDALI TERBANG OTOMATIK MENGGUNAKAN GRID FIN PADA FASE REENTRY ROKET FALCON 9

SIMULASI KENDALI TERBANG OTOMATIK MENGGUNAKAN GRID FIN PADA FASE REENTRY ROKET FALCON 9

Automatic Flight Control Simulation Using Grid Fin at Reentry Phase Falcon 9 Rocket Simulator of first stage reentry phase based on Matlab/Simulink have been made to simulate falcon 9 rocket first stage when entering earth atmosphere. This Simulator have been equipped with weight and balance, envir...

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Main Author: Chairul Akmal, Shabri
Format: Final Project
Language:Indonesia
Online Access:https://digilib.itb.ac.id/gdl/view/42915
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Institution: Institut Teknologi Bandung
Language: Indonesia
id id-itb.:42915
spelling id-itb.:429152019-09-24T14:21:49ZSIMULASI KENDALI TERBANG OTOMATIK MENGGUNAKAN GRID FIN PADA FASE REENTRY ROKET FALCON 9 Chairul Akmal, Shabri Indonesia Final Project Falcon 9, Reentry, Grid fin INSTITUT TEKNOLOGI BANDUNG https://digilib.itb.ac.id/gdl/view/42915 Automatic Flight Control Simulation Using Grid Fin at Reentry Phase Falcon 9 Rocket Simulator of first stage reentry phase based on Matlab/Simulink have been made to simulate falcon 9 rocket first stage when entering earth atmosphere. This Simulator have been equipped with weight and balance, environment, propulsion, and aerodynamic modelling which cause reentry phase attitude control effort using grid fin as control surface. Cases done in this simulation are rocket simulation without grid fin and thrust(unpowered retract simulation), rocket simulation without thrust(unpowered deploy simulation), rocket simulation without grid fin(powered retract simulation), rocket simulation with thrust and grid fin but without deflection(powered deploy simulation: grid control), and landing simulation. At those cases, we will see influences of grid fin and thrust and definite exact profil mission. text
institution Institut Teknologi Bandung
building Institut Teknologi Bandung Library
continent Asia
country Indonesia
Indonesia
content_provider Institut Teknologi Bandung
collection Digital ITB
language Indonesia
description Automatic Flight Control Simulation Using Grid Fin at Reentry Phase Falcon 9 Rocket Simulator of first stage reentry phase based on Matlab/Simulink have been made to simulate falcon 9 rocket first stage when entering earth atmosphere. This Simulator have been equipped with weight and balance, environment, propulsion, and aerodynamic modelling which cause reentry phase attitude control effort using grid fin as control surface. Cases done in this simulation are rocket simulation without grid fin and thrust(unpowered retract simulation), rocket simulation without thrust(unpowered deploy simulation), rocket simulation without grid fin(powered retract simulation), rocket simulation with thrust and grid fin but without deflection(powered deploy simulation: grid control), and landing simulation. At those cases, we will see influences of grid fin and thrust and definite exact profil mission.
format Final Project
author Chairul Akmal, Shabri
spellingShingle Chairul Akmal, Shabri
SIMULASI KENDALI TERBANG OTOMATIK MENGGUNAKAN GRID FIN PADA FASE REENTRY ROKET FALCON 9
author_facet Chairul Akmal, Shabri
author_sort Chairul Akmal, Shabri
title SIMULASI KENDALI TERBANG OTOMATIK MENGGUNAKAN GRID FIN PADA FASE REENTRY ROKET FALCON 9
title_short SIMULASI KENDALI TERBANG OTOMATIK MENGGUNAKAN GRID FIN PADA FASE REENTRY ROKET FALCON 9
title_full SIMULASI KENDALI TERBANG OTOMATIK MENGGUNAKAN GRID FIN PADA FASE REENTRY ROKET FALCON 9
title_fullStr SIMULASI KENDALI TERBANG OTOMATIK MENGGUNAKAN GRID FIN PADA FASE REENTRY ROKET FALCON 9
title_full_unstemmed SIMULASI KENDALI TERBANG OTOMATIK MENGGUNAKAN GRID FIN PADA FASE REENTRY ROKET FALCON 9
title_sort simulasi kendali terbang otomatik menggunakan grid fin pada fase reentry roket falcon 9
url https://digilib.itb.ac.id/gdl/view/42915
_version_ 1823640027137048576

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