A new computational method was developed that enables preliminary tuning of Auto Pilot System internal parameters based on time response analysis of the aircraft and its auto pilot. This method main purpose is to reduce flight tests during Auto Pilot calibration procedure.
Autopilot System Tuning
Sae Technical Papers
SAE Brasil ; 1993
1993-10-01
Conference paper
English
Ship Autopilot Tuning Using the Vishnegradskii Aizerman Diagram
British Library Conference Proceedings | 2002
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