DESIGN OF LONGITUDINAL FLIGHT CONTROL SYSTEM FOR FIGHTER AIRCRAFT USING COEFFICIENT DIAGRAM METHOD
This research discusses about creating a pitch damper, altitude hold, and speed hold controller using Coefficient Diagram Method (CDM) for aircraft type: General Dynamics F-16 Fighting Falcon. Coefficient Diagram Method is a method that uses the coefficient diagram as a vehicle to carry the characte...
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| Main Author: | |
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| Format: | Final Project |
| Language: | Indonesia |
| Online Access: | https://digilib.itb.ac.id/gdl/view/43033 |
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| Institution: | Institut Teknologi Bandung |
| Language: | Indonesia |