Methods for suppressing nonlinear oscillations in astatic auto-piloted aircraft control systems
From MaRDI portal
Publication:1745835
DOI10.1134/S1064230717030042zbMath1385.93057OpenAlexW2731129684WikidataQ109649436 ScholiaQ109649436MaRDI QIDQ1745835
Publication date: 18 April 2018
Published in: Journal of Computer and Systems Sciences International (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1134/s1064230717030042
aircraft control systemsincrease in control errorsintegrator windupweight-size and energy characteristics
Nonlinear systems in control theory (93C10) Application models in control theory (93C95) Control/observation systems governed by ordinary differential equations (93C15)
Related Items (3)
Unnamed Item ⋮ Prevention of nonlinear oscillations in system based on integral controller algorithm by the nonlinear correction method ⋮ Theory of hidden oscillations and stability of control systems
Uses Software
Cites Work
- Unnamed Item
- Unnamed Item
- Unnamed Item
- Unnamed Item
- Unnamed Item
- Unnamed Item
- Unnamed Item
- Unnamed Item
- Unnamed Item
- Unnamed Item
- Algorithms for finding hidden oscillations in nonlinear systems. The Aizerman and Kalman conjectures and Chua's circuits
- Aircraft control with anti-windup compensation
- Unloading angular momentum for inertial actuators of a spacecraft in the pitch channel
- A tutorial on modern anti-windup design
- Stabilisation and motion control of unstable objects
- Linear matrix inequalities in robustness analysis with multipliers
- A convex characterization of dynamically-constrained anti-windup controllers
- ``Neural computation of decisions in optimization problems
- Conditioning technique, a general anti-windup and bumpless transfer method
- Multiplier theory for stability analysis of anti-windup control systems
- Systematic closed-loop design in the presence of input saturations
- A unified framework for the study of anti-windup designs
- Control systems with input and output constraints
- Control of linear systems with regulation and input constraints
- An analysis and design method for linear systems subject to actuator saturation and disturbance
- Frequency criteria for the absolute stability of nonlinear sampled-data systems
- A magnitude and rate saturation model and its use in the solution of a static anti-windup problem
- Convergent dynamics, a tribute to Boris Pavlovich Demidovich
- HIDDEN ATTRACTORS IN DYNAMICAL SYSTEMS. FROM HIDDEN OSCILLATIONS IN HILBERT–KOLMOGOROV, AIZERMAN, AND KALMAN PROBLEMS TO HIDDEN CHAOTIC ATTRACTOR IN CHUA CIRCUITS
- Navigability of interconnected networks under random failures
- Stability analysis of single loop control systems with saturation and antireset-windup circuits
- Stability of discrete override and cascade-limiter single-loop control systems
- Multivariable feedback design: Concepts for a classical/modern synthesis
- A multiloop generalization of the circle criterion for stability margin analysis
- Robust receding horizon control of constrained nonlinear systems
- Linear Matrix Inequalities in System and Control Theory
- Extended anti-windup control schemes for LTI and LFT systems with actuator saturations
- A chronological bibliography on saturating actuators
- Stability and Stabilization of Linear Systems with Saturating Actuators
- Antiwindup for stable linear systems with input saturation: An LMI-based synthesis
- Formation Flying Control for Satellites: Anti-windup Based Approach
- Nonlinear Scheduled Anti-Windup Design for Linear Systems
- Antiwindup design with guaranteed regions of stability: an LMI-based approach
- Convex Design of a Robust Antiwindup Controller for an LFT Model
- Discrete-time and sampled-data anti-windup synthesis: stability and performance
- Stability Conditions for Systems with Monotone and Slope-Restricted Nonlinearities
- Non-linear anti-windup for manual flight control
- Design of Convergent Switched Systems
- Multivariable anti-windup controller synthesis using linear matrix inequalities
This page was built for publication: Methods for suppressing nonlinear oscillations in astatic auto-piloted aircraft control systems
