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...
Saved in:
| 主要作者: | |
|---|---|
| 格式: | Final Project |
| 語言: | Indonesia |
| 在線閱讀: | https://digilib.itb.ac.id/gdl/view/42915 |
| 標簽: |
添加標簽
沒有標簽, 成為第一個標記此記錄!
|
| 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 |