L1 adaptive controller of nonlinear reference system in presence of unmatched uncertainties

2016 ◽  
Vol 23 (4) ◽  
pp. 834-840 ◽  
Author(s):  
Hai-tao Song ◽  
Tao Zhang ◽  
Guo-liang Zhang
Author(s):  
Jie Luo ◽  
Chengyu Cao

This paper presents an extension of the L1 adaptive controller to a class of nonlinear systems where the control effectiveness is time-varying and unknown, but with a known sign. Moreover, this class of nonlinear systems contains time-varying and unknown state-dependent nonlinearities. The proposed L1 adaptive controller consists of three components, a state predictor used to estimate real states, an adaptive law used to update the adaptive parameters in the state predictor, and a low-pass filtered control law. First, the stable closed-loop reference system is constructed. Then, the estimation errors between estimated states and real states are proved to be arbitrarily small by increasing the adaptation rate. After that, we further prove that the adaptive controller ensures uniformly bounded transient and asymptotical tracking of the reference system. The performance bounds can be systematically improved by increasing the adaptation rate. Simulation results on a single-link nonlinear robot arm verify the theoretical findings.


Author(s):  
John Cooper ◽  
Chengyu Cao ◽  
Jiong Tang

This paper presents an L1 adaptive controller for pressure control using an engine bleed valve in an aircraft air management system (AMS). The air management system is composed of two pressure-regulating bleed valves, a temperature control valve, a flow control valve, and a heat exchanger/precooler. Valve hysteresis due to backlash and dry friction is included in the system model. The nonlinearities involved in the system cause oscillations under linear controllers, which decrease component life. This paper is the unique in the consideration of these uncertainties for control design. This paper presents simulation results using the adaptive controller and compares them to those using a proportional–integral (PI) controller.


Author(s):  
Helena Vogel ◽  
Walter Fichter ◽  
Ronald Choe ◽  
Enric Xargay ◽  
Naira Hovakimyan

Author(s):  
Z.S. Sukhov ◽  
G.A. Timofeev

This article presents a review of pneumatic, electro-pneumatic and digital systems for automatic pressure control in an airtight cabin and lists the types of aircraft where such systems are installed. Advanced algorithms for controlling the pressure in an airtight cabin are analyzed and literature on this topic is surveyed. The work of a Russian author that describes optimal control based on Pontryagin’s maximum principle is examined. The works of foreign authors on fuzzy PID-controller, L1-adaptive controller and other methods of adaptive pressurization are analyzed and brief results of these works are presented. The performed analysis indicates the need to use new methods and approaches to the synthesis of automatic pressure control systems for various types of aircraft. One of the most promising solutions is the use of adaptive regulators. The relevance of developing a virtual testing environment to reduce the cost of full-scale testing is shown.


Author(s):  
Jiang Wang ◽  
Chengyu Cao ◽  
Naira Hovakimyan ◽  
Richard Hindman ◽  
D. Brett Ridgely

2012 ◽  
Vol 35 (6) ◽  
pp. 1702-1708 ◽  
Author(s):  
Elisa Capello ◽  
Giorgio Guglieri ◽  
Daniele Sartori

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