FALCON 9 ROCKET LAUNCH SIMULATION WITH THRUST VECTORING CONTROL & OPTIMAL GUIDANCE TRAJECTORY
Falcon 9 rocket launched simulation based on MATLAB/Simulink with a complete set of coupled dynamic models of the Falcon 9 rocket, incorporating its weight and balance model, propulsion model, aerodynamics model, environmental, control and six degrees of freedom (6-DOF) equation of motion is applied...
Saved in:
| Main Author: | |
|---|---|
| Format: | Final Project |
| Language: | Indonesia |
| Online Access: | https://digilib.itb.ac.id/gdl/view/36685 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
| Institution: | Institut Teknologi Bandung |
| Language: | Indonesia |