Design for Flight Control System of UAV focused on Reliability

초록

The results show the reliabilities of DFCC, ADS and AHRS are low comparatively. The reason for DFCC is related too many integrated circuit is used in a same board. For ADS and AHRS the miro-machined sensors are the key component which drops the system reliability. To overcome this situation dual DFCC and dual AHRS will be the best tradeoff for the design of a control system of UAV. This type of design approach will be applicable to determine the configuration of a flight control system of a UAV.