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Autopilot System Tuning
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Sector:
Event:
SAE Brasil
Language:
English
Abstract
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.
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Authors
Citation
Marengo, L. and Yoneyama, T., "Autopilot System Tuning," SAE Technical Paper 931605, 1993, https://doi.org/10.4271/931605.Also In
References
- Adade Filho, A. 1984
- Etkin, B. “Dynamic of Atmospheric Flight” John Wiley & Sons New York 1972
- McRuer, D. Ashkenas, I. Graham, D. “Aircraft Dynamics and Automatic Control” Princeton University Press Princeton 1973
- Marengo, L. C. 1989
- Roskam, J. “Airplane Flight Dynamics and Automatic Flight Controls” Roskam Aviation and Corporation 1 e 2 Lawrence-Kansas 1979
- Zakian, V. Al-Naib, U. “Design of Dynamical and Control Systems by the Method of Inequalities” Proc. IEE 120 Nov. 1973 1421 1427