Aplikasi Filter KALMAN Pada Gerak Matra Longitudinal Pesawat Udara Boeing-747

Sayuti Syamsuar

Article Metrics

Abstract view : 208 times
PDF - 195 times

Abstract

Many of aircraft perfonnance became from the stability and control of flight test data analysis. This paper introduces the Kalman Filter analysis on the Boeing 747 data aircraft to knawn the output response if disturbance (as turbulence or noise) absence on the closed loop control system. We found the output response of the plant on algorithm Kalman Filter tend to the unstable conditions, but we don't knaw the response of the whole of closed loop diagram block control system of Boeing 747 aircraft.


Keywords : aircraft control system, turbulence, Kalman Filter

Full Text:

PDF

References

Dr. Mohammed AR Yass 2007, Effect c Airplane Tail Aspect Ratio on Lateral Di rectional Stability, Eng. And Technol ogy, Vol. 25, no. 6.

Katsuhiko Ogata 1970, Modem Control En gineering, Prentice Hall, Inc., N.J, USA

Copyright (c) 2019 Warta Penelitian Perhubungan
Creative Commons License
This work is licensed under a Creative Commons Attribution-NonCommercial-ShareAlike 4.0 International License.

Refbacks

  • There are currently no refbacks.

Jurnal Warta Penelitian Perhubungan have been indexed on: