Fault diagnosis and reconfiguration in flight control systems

摘要: The problem of fault diagnosis and reconfigurable control is a new actually developing field science engineering. subject becomes more interesting since there an increasing demand for the navigation systems aerospace vehicles, automated actuators etc. to be safe reliable. Nowadays, problems detection isolation attract attention scientists in world. emphasized recent international congresses such as IF AC World Congresses (San Francisco-1996, Beijing-1999, Barcelona-2002) lMEKO (Tampere-1997, Osaka-1999, Vienna-2000), also conferences on SAFEPROCESS Conferences (Hull-1997, Budapest-2000). presented methods book are based linear nonlinear dynamic mathematical models systems. Technical objects stated by these very large, include various systems, actuators, sensors, computer communication mechanical, hydraulic, pneumatic, electrical electronic devices. analytical techniques have been developed several decades. Many those use results modem theory. This natural, because it known that process considered part general process. xxii In organization concepts theory including state space, modeling, controllability, observability, estimation, identification, filtering efficient.