Linear and Nonlinear Control of Small-Scale Unmanned Helicopters (Intelligent Systems, Control and Automation: Science and Engineering) from Springer

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Product Description

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Manufacturer Description

There has actually been considerable interest for developing air travel controllers for small-scale unmanned helicopters. Such helicopters protect all the physical characteristics of their major equivalents, being at the exact same time more active and dexterous. This book presents a thorough and well justified analysis for developing air travel controllers for small-scale unmanned helicopters guarantying air travel stability and tracking accuracy. The design of the air travel controller is a vital and important part for establishing a self-governing helicopter platform. Helicopters are underactuated, extremely nonlinear systems with considerable dynamic coupling that has to be thought about and made up throughout controller design and application. Many reputable mathematical tools for analysis of control systems relate to modern-day control theory. Modern control strategies are model-based given that the controller architecture depends on the dynamic representation of the system to be controlled. Therefore, the air travel controller design issue is securely connected with the helicopter modeling.

This book offers a step-by-step approach for developing, assessing and implementing reliable air travel controllers for small-scale helicopters. Design problems that are analytically covered consist of:

• An illustrative discussion of both linear and nonlinear models of ordinary differential equations representing the helicopter characteristics. A comprehensive discussion of the helicopter equations of motion is offered for the derivation of both model types. In addition, an informative discussion of the primary rotor's system, aerodynamics and characteristics is likewise supplied. Both model types are of low complexity, physically meaningful and efficient in encapsulating the dynamic habits of a big class of small-scale helicopters.

• An illustrative and rigorous derivation of mathematical control algorithms based upon both the linear and nonlinear representation of the helicopter characteristics. Flight controller develops assurance that the tracking objectives of the helicopter's inertial position (or velocity) and heading are accomplished. Each controller is carefully built by considering the small-scale helicopter's physical air travel abilities. Ideas of innovative stability analysis are used to enhance the performance and reduce the complexity of the air travel control system. Controller designs are obtained in both constant time and discrete time covering discretization problems, which emerge from the application of the control algorithm making use of microprocessors.

• Presentation of the most effective, practical and reliable methods for extracting the helicopter model parameters based upon input/output responses, collected by the measurement instruments. This subject is of certain importance for real-life application of the control algorithms.

This book is ideal for students and looks into interested in the development and the mathematical derivation of air travel controllers for small-scale helicopters. Background knowledge in modern-day control is needed.

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