... of spacecraft simulators. Spacecraft Simulation Aerodynamics Control technology Artificial satellites © Emerald Group Publishing Limited 2010 Equation 1 The purpose of tri‐axis attitude simulator is to follow the attitude motion of satellite. To verify the effectiveness...

... as: Equation 24 Systems analysis Piezoelectricity Vibration Control technology Composite materials Plates and shells are the most widely used elements in aeronautics industry and the use of layered composite materials in the manufacturing of these parts is increasing. Still, applications...

... H_∞ control technique. Choi et al. (2000) use an almost linear model of the missile, and a robust adaptive control scheme is applied to autopilot design for feedback linearized missiles. Control technology Fourier analysis Weapons Controllers © Emerald Group...

... Group Publishing Limited 2009 Kinematics Control technology Space technology Artificial satellites As one can understand from Table I , the simulation results obtained from the first case are not feasible concerning the torque requirement levels. For the case of a microsatellite...

... for solid propellant launch and ascent vehicles. T=thrust m=mass q=pitch rate g=gravitational acceleration © Emerald Group Publishing Limited 2009 Trajectories Neural nets Control technology Aerospace engineering In this study...

... and isolated correctly. This kind of observer is also robust and flexible. © Emerald Group Publishing Limited 2008 Control technology Sensors Aircraft Failure (mechanical) Input‐output analysis In this paper, a comprehensive work on robust fault detection and identification is proposed...

... © Emerald Group Publishing Limited 2006 --> Aircraft navigation Control technology General aviation transponder Keywords: Aircraft navigation, Control technology The general aviation transponder, known as the TT31, was recently launched by Edinburgh-based Trigg...

... navigation Control technology Previous analytical studies on missile guidance problems are based on an assumption that the missile follows the proportional guidance command (Siouris, 2004). Then, the researchers try to solve a system of coupled nonlinear ordinary differential equations or apply...

... and extends the idea of supervisory controller design to cases when a special state is to be supervised while considering the effect of external disturbances. © Emerald Group Publishing Limited 2006 Aircraft navigation Aircraft components Tracking Control technology a_m...

...: Equation 33 The performance measures are: Aerospace transport Control systems Control technology A block diagram for a typical aerospace vehicle is shown in Figure 1 . The attitude of the vehicle is measured by the navigation system, and the appropriate signals are fed back...