Application of Nonlinear Correction Method for Attitude Control and Landing Oscillations Prevention

Author:

Andrievsky Boris,Zaitceva Iuliia,Kuznetsov Nikolay V.

Publisher

Elsevier BV

Subject

General Medicine

Reference28 articles.

1. Hidden oscillations in an active flutter suppression system and flight of a manned aircraft;Andrievsky;Mathematics in Engineering, Science and Aerospace,,2019

2. Hidden oscillations in aircraft flight control system with input saturation;Andrievsky;IFAC-PapersOnline,2013

3. Andrievsky, B., Arseniev, D.G., Kuznetsov, N.V., and Zaitceva, I.S. (2020). Pilot-induced oscillations and their prevention. In D.G. Arseniev, L. Overmeyer, H. K¨alvi¨ainen, and B. Katalini´c (eds.), Cyber-Physical Systems and Control, volume 95, 108–123. Springer International Publishing, Cham.

4. Methods for suppressing nonlinear oscillations in astatic auto-piloted aircraft control systems;Andrievsky;J. Computer and Systems Sciences Intern.,2017

5. Flight testing of low-order anti-windup compensators for improved handling and PIO suppression;Brieger,2008

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1. Preventing String Instability in Altitude Control System of UAV by Nonlinear Correction;2023 30th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS);2023-05-29

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