HINGE MOMENT AND CONTROL FORCE PREDICTION OF EXTRA-300 AEROBATIC AIRCRAFT
Aircraft pitch, yaw, and roll controls are controlled by elevator, rudder, and ailerons respectively. Every change in angle of attack and deflection of the surface will change the load on them. There will be a moment generated on their hinge which is transferred to the pilot through linkage system....
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| Format: | Final Project |
| Language: | Indonesia |
| Online Access: | https://digilib.itb.ac.id/gdl/view/21495 |
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| Institution: | Institut Teknologi Bandung |
| Language: | Indonesia |