MODELING AND FLIGHT CONTROL DESIGN OF A FIGHTER AIRCRAFT WITH THRUST VECTORING SYSTEM ON HIGH ANGLE OF ATTACK MANEUVER
Fighter aircraft often require unconventional maneuverability that civil aircraft cannot perform. The conventional flight control devices are not sufficient for this maneuver. Thus, to be able to perform unconventional maneuvers, additional control devices may be required, such as the thrust vec...
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| Format: | Final Project |
| Language: | Indonesia |
| Online Access: | https://digilib.itb.ac.id/gdl/view/62669 |
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| Institution: | Institut Teknologi Bandung |
| Language: | Indonesia |
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