000			01566 a2200217 4500
003			OSt
020			_a9789811087202
040			_cIIT Kanpur
041			_aeng
082			_a629.1326 _bN499f
100			_aNg, Tian Seng
245			_aFlight systems and control _ba practical approach _cTian Seng Ng
260			_bSpringer _c2018 _aSingapore
300			_axxv, 241p
440			_aSpringer aerospace technology
520			_aThis 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.
650			_aFlight control
650			_aMicroprogramming
650			_aSystems engineering
942			_cBK
999			_c566893 _d566893