Please use this identifier to cite or link to this item: http://hdl.handle.net/10603/431380
Title: Constrained Adaptive Control of Nonlinear Systems with Application to Hypersonic Vehicles
Researcher: Sachan, Kapil
Guide(s): Padhi, Radhakant
Keywords: Engineering
Engineering Aerospace
Engineering and Technology
University: Indian Institute of Science Bangalore
Completed Date: 2019
Abstract: Constraints in input, output, and states are evident in most of the practical systems. Explicitly incorporating these constraints into the control design process leads to its superior performance in general. Therefore, considering different types of constraints, several robust constrained adaptive nonlinear control designs are proposed in this thesis for different classes of uncertain nonlinear. In the first part of this thesis, a barrier Lyapunov function (BLF) based state constrained adaptive control design is presented for two different classes of uncertain nonlinear systems, known as nonlinear systems with relative degree one and Euler-Lagrange systems. In adaptive control synthesis, a neural network-based approximated system dynamics is constructed to approximate the model uncertainties of the system, and then a tracking controller is designed to achieve the desired tracking response. The weights of the neural network are updated using a Lyapunov stable weight update rule. It is shown that the closed-loop states of the system both remain bounded within the imposed constraints as well as asymptotically converge to a predefined domain. In the second part of this thesis, error transformation based state-constrained adaptive control design is proposed for generic second-order nonlinear systems with state and input constraints, model uncertainties, and external disturbances. A new error transformation is proposed to enforce state constraints; Nussbaum gain is used to impose desired input constraints, and radial basis function neural networks (RBFNNs) are utilized to approximate modeling uncertainties. In this control design philosophy, first, imposed constraints are converted into error constraints and then, using the proposed error transformation, the constrained system is transformed into equivalent unconstrained system. Next, a stable adaptive controller is designed for the unconstrained system, which indirectly establishes the stability of the constrained system without violation of imposed constraints...
Pagination: xxiv, 166p.
URI: http://hdl.handle.net/10603/431380
Appears in Departments:Aerospace Engineering

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01_title.pdfAttached File136.52 kBAdobe PDFView/Open
02_prelim pages.pdf221.9 kBAdobe PDFView/Open
03_table of content.pdf40.01 kBAdobe PDFView/Open
04_abstract.pdf28.71 kBAdobe PDFView/Open
05_chapter 1.pdf291.29 kBAdobe PDFView/Open
06_chapter 2.pdf169.85 kBAdobe PDFView/Open
07_chapter 3.pdf975.98 kBAdobe PDFView/Open
08_chapter 4.pdf1.51 MBAdobe PDFView/Open
09_chapter 5.pdf1.49 MBAdobe PDFView/Open
10_chapter 6.pdf446.92 kBAdobe PDFView/Open
11_chapter 7.pdf798.79 kBAdobe PDFView/Open
12_chapter 8.pdf1.52 MBAdobe PDFView/Open
13_annexure.pdf204.72 kBAdobe PDFView/Open
80_recommendation.pdf166.4 kBAdobe PDFView/Open
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