Flight systems and control : a practical approach
By: Ng, Tian Seng.
Series: Springer aerospace technology. Publisher: Singapore Springer 2018Description: xxv, 241p.ISBN: 9789811087202.Subject(s): Flight control | Microprogramming | Systems engineeringDDC classification: 629.1326 | N499f Summary: This book focuses on flight vehicles and their navigational systems, discussing different forms of flight structures and their control systems, from fixed wings to rotary crafts. It explores laboratory testing of flight navigational sensors, such as the magnetic, acceleration and Global Positioning System (GPS) units, and illustrates the six-axis inertial measurement unit (IMU) instrumentation as well as its data acquisition methodology. The book offers an introduction to the various unmanned aerial vehicle (UAV) systems and their accessories, including the linear quadratic regulator (LQR) method for controlling the rotorcraft. Robust control system is developed as a technique to withstand wind gusts and disturbances. It also describes a Matrix Laboratory (MATLAB) control algorithm that simulates and runs the lab- based 3 degrees of freedom (DOF) helicopter, as well as LabVIEW software used to validate controller design and data acquisition. Lastly, the book explores future developments in aviation techniques.| Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
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Books
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PK Kelkar Library, IIT Kanpur | General Stacks | 629.1326 N499f (Browse shelf) | Available | A186314 |
Browsing PK Kelkar Library, IIT Kanpur Shelves , Collection code: General Stacks Close shelf browser
| 629.1326 L112a Advanced robust nonlinear control approaches for quadrotor unmanned aerial vehicle | 629.1326 M223a AUTOMATIC FLIGHT CONTROL SYSTEMS | 629.1326 M278a Applied control systems design | 629.1326 N499f Flight systems and control | 629.1326 T31a Aeroservoelasticity | 629.1326 T31a Adaptive aeroservoelastic control | 629.1326 Un5 Unmanned aerial vehicles |
This book focuses on flight vehicles and their navigational systems, discussing different forms of flight structures and their control systems, from fixed wings to rotary crafts. It explores laboratory testing of flight navigational sensors, such as the magnetic, acceleration and Global Positioning System (GPS) units, and illustrates the six-axis inertial measurement unit (IMU) instrumentation as well as its data acquisition methodology. The book offers an introduction to the various unmanned aerial vehicle (UAV) systems and their accessories, including the linear quadratic regulator (LQR) method for controlling the rotorcraft. Robust control system is developed as a technique to withstand wind gusts and disturbances. It also describes a Matrix Laboratory (MATLAB) control algorithm that simulates and runs the lab- based 3 degrees of freedom (DOF) helicopter, as well as LabVIEW software used to validate controller design and data acquisition. Lastly, the book explores future developments in aviation techniques.
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